Showing default

COSMOS 1989 (ETALON 1), 19751

Orbit data source: Space-Track

COSMOS 1989 (ETALON 1), 19751 is a payload satellite owned by NPO PM (CIS) in MEO that was launched on Tue, 10 Jan 1989 UTC via a PROTON-K/DM-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
19751, 1989-001C
Orbit
MEO
Country
Flag of CISCIS
Related business
Manufacturer
OAZ?
Mission
Operational Defense Geodetic
Bus & Motor
ETALON, Unknown motor
Mass
1,230 kg wet, 1,230 kg dry
Launch date (UTC)
1989-01-10 (37 years ago)
Launch vehicle
PROTON-K/DM-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere, 0.6 m
Radar Cross Section
1.307 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 22 hours ago

TLE from 22 hours ago
0 COSMOS 1989 (ETALON 1)
1 19751U 89001C   25348.41379716 -.00000056  00000-0  00000-0 0  9993
2 19751  64.8366  78.5199 0023437 217.1741 160.2553  2.13156032287438
Epoch: 2025-12-14T09:55Z
TLE epoch observation values (Epoch: 2025-12-14T09:55:52.074Z)
Latitude
15.82753°
Longitude
-146.13563°
Altitude
19,181.961 km
Speed
3.945 km/s
True Right ascension
05h 44m 38s
True Declination
15° 48' 09"
Sunlit
Object was in full shadow 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
06:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,184.969 km
Perigee altitude
19,065.425 km
Semi-major axis
25,503.334 km
Eccentricity
0.00234
Inclination
64.8366°
RAAN
78.5199°
Arg. of periapsis
217.1741°
True anomaly
160.34578°
Mean anomaly
160.2553°
Eccentric anomaly
160.30057°
Mean motion
0.5329 °/min
Orbital period
675.55 mins
BSTAR
0
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
|