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). Payloads include a variety of satellites, spacecraft, and rockets 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)
REFLECTOR details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 5 hours ago |
| Origin | |
| 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 | Payload Rocket body Debris |
| Shape & HBR | Box + 4 Fin, 1.4 m |
| Radar Cross Section | 1.680 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 5 hours ago
0 REFLECTOR
1 27005U 01056E 24361.47326476 .00000259 00000-0 33971-3 0 9993
2 27005 99.7022 153.5121 0018773 58.3685 301.9290 13.71260903152839Epoch: 2024-12-26T11:21Z
Definitive object data (Epoch: 2024-12-26T11:21:30.075Z)
| Latitude | 0.00001° |
| Longitude | -112.31537° |
| Altitude | 990.559 km |
| Speed | 7.36 km/s |
| True Right ascension | 10h 14m 02s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -75.67603° |
| Longitude | 26.11601° |
| Altitude | 1,035.264 km |
| Speed | 7.327 km/s |
| Apparent Right ascension | 02h 02m 12s |
| Apparent Declination | -69° 10' 10" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 15:29:21 |
| Azimuth | 165.351° S |
| Elevation | -58.537° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,006.157 km |
| Perigee altitude | 978.484 km |
| Semi-major axis | 7,370.458 km |
| Eccentricity | 0.0018773 |
| Inclination | 99.7022° |
| RAAN | 153.5121° |
| Arg. of periapsis | 58.3685° |
| True anomaly | 301.7462° |
| Mean anomaly | 301.929° |
| Eccentric anomaly | 301.83762° |
| Mean motion | 3.43006 °/min |
| BSTAR | 0.00033971 |
| Orbital period | 104.95 mins |
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Other satellites on launch #56 in the year 2001 (2001-12-10 UTC)
REFLECTOR Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2024-12-26 22:28:14.762Z | 37.043° NE | 2024-12-26 22:33:14.762Z | 101.772° ESE | 29.582° | 2024-12-26 22:38:14.762Z | 160.217° S |
| 9 mins | 2024-12-27 00:12:14.762Z | 352.106° N | 2024-12-27 00:16:14.762Z | 300.254° NW | 30.781° | 2024-12-27 00:21:14.762Z | 233.582° WSW |
| 4 mins | 2024-12-27 08:35:14.762Z | 70.07° E | 2024-12-27 08:36:14.762Z | 59.281° ENE | 14.096° | 2024-12-27 08:39:14.762Z | 28.53° NE |
| 11 mins | 2024-12-27 10:14:14.762Z | 162.923° S | 2024-12-27 10:19:14.762Z | 15.677° NNE | 44.979° | 2024-12-27 10:25:14.762Z | 345.613° N |
Authenticating...
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