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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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: 7 hours ago
TLE from 7 hours ago
0 REFLECTOR
1 27005U 01056E 26214.64426865 .00000168 00000-0 23857-3 0 9995
2 27005 99.7698 25.7864 0018277 357.8116 2.2948 13.71457787232903Epoch: 2026-08-02T15:27Z
TLE epoch observation values (Epoch: 2026-08-02T15:27:44.811Z)
Latitude
0.00006°
Longitude
-157.38909°
Altitude
983.688 km
Speed
7.367 km/s
True Right ascension
01h 43m 08s
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
12:05:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,005.088 km
Perigee altitude
978.149 km
Semi-major axis
7,369.755 km
Eccentricity
0.00183
Inclination
99.7698°
RAAN
25.7864°
Arg. of periapsis
357.8116°
True anomaly
2.30321°
Mean anomaly
2.2948°
Eccentric anomaly
2.299°
Mean motion
3.43055 °/min
Orbital period
104.94 mins
BSTAR
0.00023857
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-08-02 23:05:49.425Z | 54.341° ENE | 2026-08-02 23:09:49.425Z | 99.357° ESE | 18.793° | 2026-08-02 23:12:49.425Z | 131.629° SE |
| 10 mins | 2026-08-03 00:48:49.425Z | 4.301° NNE | 2026-08-03 00:52:49.425Z | 309.531° NW | 41.148° | 2026-08-03 00:58:49.425Z | 211.301° SW |
| 10 mins | 2026-08-03 10:50:49.425Z | 140.797° SSE | 2026-08-03 10:55:49.425Z | 62.382° ENE | 38.555° | 2026-08-03 11:00:49.425Z | 356.757° N |
| 8 mins | 2026-08-03 12:35:49.425Z | 222.812° SW | 2026-08-03 12:39:49.425Z | 271.317° WNW | 21.395° | 2026-08-03 12:43:49.425Z | 314.499° NW |
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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