OV1-5, 2122
Orbit data source: Space-Track
OV1-5, 2122 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Wed, 30 Mar 1966 UTC via an ATLAS 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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2122 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
GD/Convair
Mission
Spacecraft
Bus & Motor
OV1, Unknown motor
Mass
114 kg wet, 114 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 OV1-5
1 02122U 66025B 25340.24609728 .00000338 00000-0 94586-4 0 9998
2 02122 144.6344 84.7666 0047250 18.9070 341.3351 13.66144228978714Epoch: 2025-12-06T05:54Z
TLE epoch observation values (Epoch: 2025-12-06T05:54:22.804Z)
Latitude
-0.00003°
Longitude
-79.10497°
Altitude
979.401 km
Speed
7.38 km/s
True Right ascension
05h 39m 03s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
15:49:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,051.355 km
Perigee altitude
981.477 km
Semi-major axis
7,394.553 km
Eccentricity
0.00473
Inclination
144.6344°
RAAN
84.7666°
Arg. of periapsis
18.907°
True anomaly
341.16085°
Mean anomaly
341.3351°
Eccentric anomaly
341.24807°
Mean motion
3.41331 °/min
Orbital period
105.47 mins
BSTAR
0.000094586
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Other satellites on launch #25 in the year 1966 (1966-03-30 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.OV1-5 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-12-06 22:14:54.605Z | 104.479° ESE | 2025-12-06 22:18:54.605Z | 147.817° SSE | 21.047° | 2025-12-06 22:22:54.605Z | 196.126° SSW |
| 10 mins | 2025-12-06 23:54:54.605Z | 99.225° ESE | 2025-12-06 23:58:54.605Z | 155.825° SSE | 34.96° | 2025-12-07 00:04:54.605Z | 236.686° WSW |
| 9 mins | 2025-12-07 01:34:54.605Z | 104.292° ESE | 2025-12-07 01:38:54.605Z | 174.075° S | 40.637° | 2025-12-07 01:43:54.605Z | 255.212° W |
| 9 mins | 2025-12-07 03:14:54.605Z | 124.994° SE | 2025-12-07 03:18:54.605Z | 197.054° SSW | 37.192° | 2025-12-07 03:23:54.605Z | 264.566° W |
| 7 mins | 2025-12-07 04:55:54.605Z | 164.243° S | 2025-12-07 04:58:54.605Z | 207.811° SW | 24.33° | 2025-12-07 05:02:54.605Z | 256.338° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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