REFLECTOR, 27005
Orbit data source: Space-Track
REFLECTOR, 27005 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Mon, 10 Dec 2001 UTC via a ZENIT-2 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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27005 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NIIPP
Mission
Defense Calibration
Bus & Motor
REFLEKTOR, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 4 Fin, 0.7 m
Radar Cross Section
1.680 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 REFLECTOR
1 27005U 01056E 25310.29507965 .00000101 00000-0 16395-3 0 9999
2 27005 99.7433 112.2018 0017938 328.9023 31.1060 13.71383006195986Epoch: 2025-11-06T07:04Z
TLE epoch observation values (Epoch: 2025-11-06T07:04:54.881Z)
Latitude
-0.00005°
Longitude
-39.78231°
Altitude
986.104 km
Speed
7.364 km/s
True Right ascension
07h 28m 48s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:54:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,005.105 km
Perigee altitude
978.665 km
Semi-major axis
7,370.022 km
Eccentricity
0.00179
Inclination
99.7433°
RAAN
112.2018°
Arg. of periapsis
328.9023°
True anomaly
31.2124°
Mean anomaly
31.106°
Eccentric anomaly
31.15918°
Mean motion
3.43036 °/min
Orbital period
104.95 mins
BSTAR
0.00016395
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Other satellites on launch #56 in the year 2001 (2001-12-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.REFLECTOR Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-11-06 23:25:39.566Z | 24.542° NE | 2025-11-06 23:31:39.566Z | 108.492° ESE | 39.36° | 2025-11-06 23:36:39.566Z | 176.37° S |
| 7 mins | 2025-11-07 01:11:39.566Z | 335.197° NNW | 2025-11-07 01:14:39.566Z | 297.101° NW | 22.648° | 2025-11-07 01:18:39.566Z | 251.793° W |
| 7 mins | 2025-11-07 09:31:39.566Z | 93.685° ESE | 2025-11-07 09:34:39.566Z | 55.459° ENE | 21.039° | 2025-11-07 09:38:39.566Z | 13.6° NNE |
| 10 mins | 2025-11-07 11:12:39.566Z | 182.437° SSW | 2025-11-07 11:17:39.566Z | 272.788° WNW | 40.376° | 2025-11-07 11:22:39.566Z | 335.648° NNW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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