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: 19 hours ago
TLE from 19 hours ago
0 OV1-5
1 02122U 66025B 26038.40075262 .00000343 00000-0 10029-3 0 9996
2 02122 144.6380 31.5060 0046687 96.5888 264.0099 13.66154991987352Epoch: 2026-02-07T09:37Z
TLE epoch observation values (Epoch: 2026-02-07T09:37:05.026Z)
Latitude
-0.00002°
Longitude
109.71028°
Altitude
1,016.186 km
Speed
7.344 km/s
True Right ascension
02h 06m 01s
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
07:01:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,050.901 km
Perigee altitude
981.855 km
Semi-major axis
7,394.515 km
Eccentricity
0.00467
Inclination
144.638°
RAAN
31.506°
Arg. of periapsis
96.5888°
True anomaly
263.47816°
Mean anomaly
264.0099°
Eccentric anomaly
263.744°
Mean motion
3.41333 °/min
Orbital period
105.47 mins
BSTAR
0.00010029
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-02-08 14:17:04.110Z | 116.939° SE | 2026-02-08 14:20:04.110Z | 150.659° SSE | 16.369° | 2026-02-08 14:23:04.110Z | 184.257° SSW |
| 9 mins | 2026-02-08 15:56:04.110Z | 101.658° ESE | 2026-02-08 16:00:04.110Z | 160.481° S | 31.682° | 2026-02-08 16:05:04.110Z | 227.093° WSW |
| 9 mins | 2026-02-08 17:36:04.110Z | 102.721° ESE | 2026-02-08 17:40:04.110Z | 179.325° S | 39.95° | 2026-02-08 17:45:04.110Z | 251.598° W |
| 10 mins | 2026-02-08 19:15:04.110Z | 114.972° SE | 2026-02-08 19:20:04.110Z | 201.705° SSW | 38.625° | 2026-02-08 19:25:04.110Z | 264.266° W |
| 8 mins | 2026-02-08 20:56:04.110Z | 149.513° SSE | 2026-02-08 21:00:04.110Z | 210.423° SW | 28.084° | 2026-02-08 21:04:04.110Z | 259.561° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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