Showing default

COSMOS 2269, 23000

Orbit data source: Space-Track

COSMOS 2269, 23000 is a payload satellite owned by VKS (CIS) in LEO that was launched on Sat, 12 Feb 1994 UTC via a TSIKLON-3 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
23000, 1994-011B
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
1994-02-12 (32 years ago)
Launch vehicle
TSIKLON-3
Launch site
Plesetsk Missile And Space Complex (PKMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
1.257 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 19 hours ago

TLE from 19 hours ago
0 COSMOS 2269
1 23000U 94011B   25295.91554594  .00000016  00000-0  32289-4 0  9990
2 23000  82.5630 112.6385 0007220  14.6221 162.8895 12.61935998459745
Epoch: 2025-10-22T21:58Z
TLE epoch observation values (Epoch: 2025-10-22T21:58:23.169Z)
Latitude
2.34855°
Longitude
-68.84556°
Altitude
1,422.797 km
Speed
7.147 km/s
True Right ascension
19h 29m 19s
True Declination
2° 20' 09"
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
12:17:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,417.91 km
Perigee altitude
1,406.661 km
Semi-major axis
7,790.423 km
Eccentricity
0.00072
Inclination
82.563°
RAAN
112.6385°
Arg. of periapsis
14.6221°
True anomaly
162.91382°
Mean anomaly
162.8895°
Eccentric anomaly
162.90166°
Mean motion
3.15647 °/min
Orbital period
114.05 mins
BSTAR
0.000032289
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
|