Showing default

OPS 1920, 2481

Orbit data source: Space-Track

OPS 1920, 2481 is a payload satellite owned by USAF SSD (US) in LEO that was launched on Wed, 05 Oct 1966 UTC via an ATLAS SLV-3 AGENA D 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
2481, 1966-089A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
LMSC
Mission
Defense Early Warn
Bus & Motor
MIDAS, Unknown motor
Mass
~2,000 kg wet, ~1,000 kg dry
Launch date (UTC)
1966-10-05 (59 years ago)
Launch vehicle
ATLAS SLV-3 AGENA D
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cone + Cyl + 2 Pan, 1.5 m
Radar Cross Section
4.418 m², Large (>1 m²)

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

TLE from 1 day ago
0 OPS 1920
1 02481U 66089A   25259.31649658 -.00000003  00000-0 -24285-2 0  9997
2 02481  89.8341  32.9518 0032321 233.1806 126.6079  8.59254045849141
Epoch: 2025-09-16T07:35Z
TLE epoch observation values (Epoch: 2025-09-16T07:35:45.304Z)
Latitude
0.00003°
Longitude
-76.49551°
Altitude
3,712.551 km
Speed
6.28 km/s
True Right ascension
02h 11m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full 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
02:55:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,721.245 km
Perigee altitude
3,656.171 km
Semi-major axis
10,066.845 km
Eccentricity
0.00323
Inclination
89.8341°
RAAN
32.9518°
Arg. of periapsis
233.1806°
True anomaly
126.90449°
Mean anomaly
126.6079°
Eccentric anomaly
126.75627°
Mean motion
2.14884 °/min
Orbital period
167.53 mins
BSTAR
-0.0024285
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 #89 in the year 1966 (1966-10-05 UTC)

Documentation

Showing up to 5 results
|