Showing default

COSMOS 2076, 20596

Orbit data source: Space-Track

COSMOS 2076, 20596 is a payload satellite owned by PVO (CIS) in HEO that was launched on Sat, 28 Apr 1990 UTC via an MOLNIYA 8K78M 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
20596, 1990-040A
Orbit
HEO
Country
Flag of CISCIS
Related business
Manufacturer
NPOL/KOMET
Mission
Defense Early Warn
Bus & Motor
OKO, Unknown motor
Mass
~1,250 kg wet, ~1,150 kg dry
Launch date (UTC)
1990-04-28 (36 years ago)
Launch vehicle
MOLNIYA 8K78M
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan, 2.5 m
Radar Cross Section
6.333 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 months ago

TLE from 9 months ago
0 COSMOS 2076
1 20596U 90040A   25259.55383186  .00000018  00000-0  00000+0 0  9995
2 20596  68.6654 210.2926 4874395 113.6019  23.9114  2.00705145259260
Epoch: 2025-09-16T13:17Z
TLE epoch observation values (Epoch: 2025-09-16T13:17:31.072Z)
Latitude
-1.39187°
Longitude
-164.29153°
Altitude
10,706.526 km
Speed
5.626 km/s
True Right ascension
02h 03m 19s
True Declination
-1° 23' 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
18:28:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,109.104 km
Perigee altitude
7,228.87 km
Semi-major axis
26,547.124 km
Eccentricity
0.48744
Inclination
68.6654°
RAAN
210.2926°
Arg. of periapsis
113.6019°
True anomaly
67.63816°
Mean anomaly
23.9114°
Eccentric anomaly
42.93534°
Mean motion
0.50178 °/min
Orbital period
717.44 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
|