Showing default

COSMOS 1925, 18938

Orbit data source: Space-Track

COSMOS 1925, 18938 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Fri, 11 Mar 1988 UTC via a KOSMOS 11K65M launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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
18938, 1988-016B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-1 11F625, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
1988-03-11 (38 years ago)
Launch vehicle
KOSMOS 11K65M
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere, 0.4 m
Radar Cross Section
0.588 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 COSMOS 1925
1 18938U 88016B   25347.02010123 -.00000005  00000-0  75712-4 0  9994
2 18938  74.0059 298.4864 0024860 244.7410 184.2324 12.46846311718577
Epoch: 2025-12-13T00:28Z
TLE epoch observation values (Epoch: 2025-12-13T00:28:56.746Z)
Latitude
63.87815°
Longitude
-115.1351°
Altitude
1,507.823 km
Speed
7.108 km/s
True Right ascension
22h 16m 13s
True Declination
63° 45' 18"
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
05:22:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,495.079 km
Perigee altitude
1,456.03 km
Semi-major axis
7,853.691 km
Eccentricity
0.00249
Inclination
74.0059°
RAAN
298.4864°
Arg. of periapsis
244.741°
True anomaly
184.21144°
Mean anomaly
184.2324°
Eccentric anomaly
184.22191°
Mean motion
3.1184 °/min
Orbital period
115.44 mins
BSTAR
0.000075712
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
|