Showing default

OPS 7202 (DMSP 4A F3), 2920

Orbit data source: Space-Track

OPS 7202 (DMSP 4A F3), 2920 is a payload satellite owned by SAMSO (US) in SSO that was launched on Wed, 23 Aug 1967 UTC via a THOR BURNER 2 launch vehicle from the Air Force Western Test Range (AFWTR). 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
2920, 1967-080A
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
RCA/East Windsor
Mission
Non-operational spacecraft
Bus & Motor
DMSP BLOCK 4A, Unknown motor
Mass
79 kg wet, 79 kg dry
Launch date (UTC)
1967-08-23 (59 years ago)
Launch vehicle
THOR BURNER 2
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 OPS 7202 (DMSP 4A F3)
1 02920U 67080A   26145.29610239  .00000033  00000-0  38266-4 0  9999
2 02920  98.5890 356.0638 0039025  63.5937 296.9234 14.15305053 29471
Epoch: 2026-05-25T07:06Z
TLE epoch observation values (Epoch: 2026-05-25T07:06:23.246Z)
Latitude
-0.00008°
Longitude
6.58102°
Altitude
831.515 km
Speed
7.444 km/s
True Right ascension
23h 44m 15s
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
17:17:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
866.596 km
Perigee altitude
810.271 km
Semi-major axis
7,216.571 km
Eccentricity
0.0039
Inclination
98.589°
RAAN
356.0638°
Arg. of periapsis
63.5937°
True anomaly
296.5238°
Mean anomaly
296.9234°
Eccentric anomaly
296.72369°
Mean motion
3.54036 °/min
Orbital period
101.68 mins
BSTAR
0.000038266
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...
Other satellites on launch #80 in the year 1967 (1967-08-23 UTC)

Documentation

Showing up to 5 results
|