Showing default

COSMOS 249, 3504

Orbit data source: Space-Track

COSMOS 249, 3504 is a payload satellite owned by PKO (CIS) in LEO that was launched on Sun, 20 Oct 1968 UTC via a TSIKLON-2A 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
3504, 1968-091A
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
TSKBM/KB1
Mission
Spacecraft
Bus & Motor
IS, Unknown motor
Mass
1,400 kg wet, ~1,400 kg dry
Launch date (UTC)
1968-10-20 (57 years ago)
Launch vehicle
TSIKLON-2A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)

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

TLE from 19 hours ago
0 COSMOS 249
1 03504U 68091A   25310.13131013  .00000040  00000-0  48984-4 0  9991
2 03504  62.3484 107.2531 0992155 335.7291  19.9835 12.97004956691555
Epoch: 2025-11-06T03:09Z
TLE epoch observation values (Epoch: 2025-11-06T03:09:05.195Z)
Latitude
-0.00003°
Longitude
14.38741°
Altitude
572.191 km
Speed
7.915 km/s
True Right ascension
07h 09m 00s
True Declination
0° 00' 00"
Sunlit
Object was in partial 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
18:12:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,031.912 km
Perigee altitude
513.725 km
Semi-major axis
7,650.956 km
Eccentricity
0.09922
Inclination
62.3484°
RAAN
107.2531°
Arg. of periapsis
335.7291°
True anomaly
24.37404°
Mean anomaly
19.9835°
Eccentric anomaly
22.12444°
Mean motion
3.24317 °/min
Orbital period
111 mins
BSTAR
0.000048984
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|