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: 13 hours ago
TLE from 13 hours ago
0 OV1-5
1 2122U 66025B 25295.07280719 .00000386 00000-0 15184-3 0 9992
2 2122 144.6350 225.3522 0046733 66.8599 293.6990 13.66135925972534Epoch: 2025-10-22T01:44Z
TLE epoch observation values (Epoch: 2025-10-22T01:44:50.541Z)
Latitude
-0.00002°
Longitude
168.38998°
Altitude
998.75 km
Speed
7.361 km/s
True Right ascension
15h 01m 24s
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
10:14:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,051.003 km
Perigee altitude
981.889 km
Semi-major axis
7,394.583 km
Eccentricity
0.00467
Inclination
144.635°
RAAN
225.3522°
Arg. of periapsis
66.8599°
True anomaly
293.20749°
Mean anomaly
293.699°
Eccentric anomaly
293.45336°
Mean motion
3.41329 °/min
Orbital period
105.47 mins
BSTAR
0.00015184
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-10-22 16:01:27.153Z | 127.676° SE | 2025-10-22 16:06:27.153Z | 195.493° SSW | 33.897° | 2025-10-22 16:11:27.153Z | 264.015° W |
| 7 mins | 2025-10-22 17:43:27.153Z | 170.785° S | 2025-10-22 17:46:27.153Z | 207.022° SW | 19.18° | 2025-10-22 17:50:27.153Z | 252.259° W |
| 8 mins | 2025-10-23 11:36:27.153Z | 109.56° ESE | 2025-10-23 11:39:27.153Z | 153.543° SSE | 28.161° | 2025-10-23 11:44:27.153Z | 218.646° SW |
| 9 mins | 2025-10-23 13:15:27.153Z | 100.193° ESE | 2025-10-23 13:19:27.153Z | 165.771° S | 38.82° | 2025-10-23 13:24:27.153Z | 245.633° WSW |
| 9 mins | 2025-10-23 14:55:27.153Z | 112.737° SE | 2025-10-23 14:59:27.153Z | 189.189° SSW | 39.979° | 2025-10-23 15:04:27.153Z | 261.727° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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