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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.

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Identifier
2481, 1966-089A
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
LMSC
Mission
Spacecraft
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
Unknown
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 OPS 1920
1  2481U 66089A   25344.53455046  .00000003  00000-0  55631-3 0  9990
2  2481  89.8369  32.4547 0033046 148.8862 211.3954  8.59255013856460
Epoch: 2025-12-10T12:49Z
TLE epoch observation values (Epoch: 2025-12-10T12:49:45.159Z)
Latitude
-0.00001°
Longitude
120.51304°
Altitude
3,721.502 km
Speed
6.274 km/s
True Right ascension
02h 09m 49s
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
01:14:56
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
3,721.968 km
Perigee altitude
3,655.434 km
Semi-major axis
10,066.838 km
Eccentricity
0.0033
Inclination
89.8369°
RAAN
32.4547°
Arg. of periapsis
148.8862°
True anomaly
211.19882°
Mean anomaly
211.3954°
Eccentric anomaly
211.29704°
Mean motion
2.14884 °/min
Orbital period
167.53 mins
BSTAR
0.00055631
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Other satellites on launch #89 in the year 1966 (1966-10-05 UTC)

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