BRIGHTNESS SCALE

Magnitude Comparisons — All Mirrors

Astronomical apparent magnitude is a logarithmic scale. Each step of 1 magnitude represents a brightness factor of ~2.5×. Lower (and negative) numbers are brighter. The scale below places all orbital mirror missions in context.

−26.7
The Sun
Reference point for solar illumination
−12.7
Full Moon
Bright enough to cast shadows; disrupts dark adaptation
−10 to −12
Tumbling Mirror (worst case)
Uncontrolled large-area reflector flare — brighter than full Moon, globally visible for seconds
−4.6
Venus (maximum)
Visible in daylight; easily seen at dusk/dawn; casts faint shadow
~−4 to −5
EARENDIL-1 (peak, overhead)
Comparable to Venus at its brightest — conspicuous at dusk, visible to naked eye as moving point
−1.5
Sirius (brightest star)
Reference for "very bright star"
~3
Znamya-2 (1993, actual)
Visible to naked eye as a faint moving object. Traced across Europe during the 1993 demonstration
~3
Znamya-2.5 target (1999)
Intended magnitude before deployment failure. Comparable to a moderately bright star
3–5
Typical ISS / Starlink flare
Common point of comparison for existing satellite brightness
IMPORTANT NOTE ON EARENDIL-1 BRIGHTNESS
Reflect Orbital's stated target brightness for EARENDIL-1 is approximately Venus-equivalent (magnitude ~−4) when the mirror is directly overhead and optimally oriented. At lower elevations or non-optimal angles, apparent brightness drops significantly. The mirror is designed to be steerable — it can be tilted away from Earth between targeted passes, meaning it would not be continuously bright like a flat reflective surface.
FOOTPRINT DATA

How Large Is the Illuminated Area?

~5kmZNAMYA-2 · 1993Traced across European cities during demonstration pass
~5kmEARENDIL-1 · 2026Design target. Comparable to a city district. Moves at ~7.6km/s ground speed
50km+CHENGDU PROPOSAL · 2018Claimed urban illumination footprint — technically disputed

The 5km footprint figure for EARENDIL-1 represents the region receiving meaningful supplemental illumination. The reflector is 18×18m, which from 625km altitude subtends a very small angle. The mirror is not focusing sunlight to a tight point (that would require a concentrating rather than flat reflector); instead it produces a relatively diffuse 5km beam of enhanced ambient light.

FLARE RISK

The Tumbling Mirror Scenario

RISK SCENARIO · WORST CASE
If an orbital mirror loses attitude control and begins tumbling, it becomes an uncontrolled specular reflector sweeping the sunlit side of Earth with a rapidly rotating beam. Depending on geometry, peak flares could reach magnitude −10 to −12 — comparable to or brighter than the full Moon — lasting several seconds per rotation cycle. A mirror at 625km altitude in a stable orbit without active deorbit capability could remain in orbit for months to years. Unlike a communications satellite failure, which is invisible, a tumbling mirror failure is visible to the entire hemisphere it is over.

This risk is not theoretical. In 2024, NASA's Advanced Composite Solar Sail System (ACS3) — a technology demonstration satellite deploying a large reflective sail — began rotating uncontrollably after deployment. ACS3's reflective area is much smaller than EARENDIL-1's proposed mirror and is not optimised for maximum reflectivity toward Earth. Despite this, the failure mode was real and public.

Reflect Orbital has described attitude control as a core technical challenge but has not published detailed failure mode analysis in the public domain. The FCC experimental licence does not appear to have required this analysis as a condition of approval.

OBSERVATION GUIDE

What Would You Actually See?

MIRROR EXPECTED APPEARANCE DURATION FREQUENCY NAKED EYE?
Znamya-2 (1993) Faint moving point, mag ~3–5 ~5 min per pass Single demo YES
EARENDIL-1 (planned) Bright moving point, mag ~−4 to −5 near zenith ~3.5 min per pass Multiple daily (targeted) YES — bright
4,000-sat constellation Near-continuous brightening of sky background; multiple simultaneous passes Ongoing Continuous over target regions YES — pervasive
Tumbling mirror (worst case) Multi-second flares, mag −10 to −12 — brighter than full Moon Seconds per flare cycle Until deorbit (months–years) YES — alarming