Showing default

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.

Loading next visibility...
Identifier
27005, 2001-056E
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
NIIPP
Mission
Defense Calibration
Bus & Motor
REFLEKTOR, Unknown motor
Mass
8 kg wet, 8 kg dry
Launch date (UTC)
2001-12-10 (24 years ago)
Launch vehicle
ZENIT-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
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 & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 REFLECTOR
1 27005U 01056E   25365.59611801  .00000108  00000-0  17129-3 0  9990
2 27005  99.7446 168.3109 0018380 183.4130 176.6894 13.71403303203565
Epoch: 2025-12-31T14:18Z
TLE epoch observation values (Epoch: 2025-12-31T14:18:24.596Z)
Latitude
0.00005°
Longitude
-146.55437°
Altitude
1,010.882 km
Speed
7.34 km/s
True Right ascension
11h 13m 14s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
20:14:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,005.358 km
Perigee altitude
978.266 km
Semi-major axis
7,369.949 km
Eccentricity
0.00184
Inclination
99.7446°
RAAN
168.3109°
Arg. of periapsis
183.413°
True anomaly
176.70154°
Mean anomaly
176.6894°
Eccentric anomaly
176.69547°
Mean motion
3.43041 °/min
Orbital period
104.94 mins
BSTAR
0.00017129
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|