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DECAYED
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OV4-IT, 2528 (Decayed)

Orbit data source: Public

OV4-IT, 2528 was an American payload satellite that was launched on Thu, 03 Nov 1966 UTC via a TITAN IIIC launch vehicle from the Air Force Eastern Test Range (AFETR). Payloads include a variety of satellites, spacecraft, and rockets 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.

Next visibility unknown
No 3D visualization available: No data
OV4-IT details
Identifier
2528, 1966-099D
Orbit
Decayed
Last TLE updateUnknown
Origin
Flag of USOAR/AFSSD (US)
ManufacturerRaytheon
MissionDecayed Defense Technology
Bus & MotorOV4, UNK
Mass109 kg wet, 109 kg dry
Launch date (UTC)
1966-11-03 (58 years ago)
Launch vehicle
TITAN IIIC
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBRCyl, 1.4 m
Radar Cross Section0.503 m²

Expand to show TLE details & history

Definitive object data
LatitudeUnknown
LongitudeUnknown
AltitudeUnknown
SpeedUnknown
True Right ascensionUnknown
True DeclinationUnknown
Sunlit
Object was in daylight at TLE epoch
Predictive object data (real-time)
LatitudeUnknown
LongitudeUnknown
AltitudeUnknown
SpeedUnknown
Apparent Right ascensionUnknown
Apparent DeclinationUnknown
SunlitUnknown
Predictive observer data (real-time)
Local Sidereal Time18:02:23
AzimuthUnknown
ElevationUnknown
Doppler factorUnknown
Orbital elements
ApogeeUnknown
PerigeeUnknown
Semi-major axisUnknown
EccentricityUnknown
InclinationUnknown
RAANUnknown
Arg. of periapsisUnknown
True anomalyUnknown
Mean anomalyUnknown
Eccentric anomalyUnknown
Mean motionUnknown
BSTARUnknown
PeriodUnknown
No data available
No data available

OV4-IT Visibility forecast

Observer location: 39.9160978°, -105.1181434

This satellite is decayed
Span
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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.