Showing default

COSMOS 252, 3530

Orbit data source: Space-Track

COSMOS 252, 3530 is a payload satellite owned by PKO (CIS) in LEO that was launched on Fri, 01 Nov 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
3530, 1968-097A
Orbit
LEO
Country
Flag of CISCIS
Related business
Manufacturer
TSKBM/KB1
Mission
Defense Weapon
Bus & Motor
IS, Unknown motor
Mass
1,400 kg wet, ~1,400 kg dry
Launch date (UTC)
1968-11-01 (57 years ago)
Launch vehicle
TSIKLON-2A
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 2.0 m
Radar Cross Section
7.854 m², Large (>1 m²)

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

TLE from 22 hours ago
0 COSMOS 252
1 03530U 68097A   25242.12051351  .00000255  00000-0  14337-3 0  9997
2 03530  62.3247 147.4911 0990937 355.8150   3.4979 12.88167519668457
Epoch: 2025-08-30T02:53Z
TLE epoch observation values (Epoch: 2025-08-30T02:53:32.367Z)
Latitude
0.00004°
Longitude
125.54689°
Altitude
550.425 km
Speed
7.953 km/s
True Right ascension
09h 49m 57s
True Declination
0° 00' 00"
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
16:21:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
2,069.41 km
Perigee altitude
546.158 km
Semi-major axis
7,685.921 km
Eccentricity
0.09909
Inclination
62.3247°
RAAN
147.4911°
Arg. of periapsis
355.815°
True anomaly
4.28778°
Mean anomaly
3.4979°
Eccentric anomaly
3.88232°
Mean motion
3.22106 °/min
Orbital period
111.76 mins
BSTAR
0.00014337
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|