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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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
DOMED CYL, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 16 hours ago
TLE from 16 hours ago
0 OV1-5
1 02122U 66025B 26290.64980284 .00000310 00000-0 60752-4 0 9994
2 02122 144.6336 176.7418 0046946 41.2661 319.1551 13.66181045 21822Epoch: 2026-10-17T15:35Z
TLE epoch observation values (Epoch: 2026-10-17T15:35:42.965Z)
Latitude
0.00003°
Longitude
-83.34069°
Altitude
986.158 km
Speed
7.374 km/s
True Right ascension
11h 46m 58s
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
02:01:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,050.997 km
Perigee altitude
981.569 km
Semi-major axis
7,394.42 km
Eccentricity
0.00469
Inclination
144.6336°
RAAN
176.7418°
Arg. of periapsis
41.2661°
True anomaly
318.8017°
Mean anomaly
319.1551°
Eccentric anomaly
318.97856°
Mean motion
3.4134 °/min
Orbital period
105.47 mins
BSTAR
0.000060752
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-10-18 07:54:57.751Z | 100.69° ESE | 2026-10-18 07:59:57.751Z | 159.036° S | 25.934° | 2026-10-18 08:03:57.751Z | 205.895° SW |
| 9 mins | 2026-10-18 09:35:57.751Z | 102.375° ESE | 2026-10-18 09:39:57.751Z | 177.345° S | 47.932° | 2026-10-18 09:44:57.751Z | 239.776° WSW |
| 10 mins | 2026-10-18 11:14:57.751Z | 104.762° ESE | 2026-10-18 11:18:57.751Z | 160.921° S | 58.103° | 2026-10-18 11:24:57.751Z | 259.573° W |
| 9 mins | 2026-10-18 12:54:57.751Z | 127.065° SE | 2026-10-18 12:58:57.751Z | 187.753° SSW | 46.137° | 2026-10-18 13:03:57.751Z | 263.546° W |
| 7 mins | 2026-10-18 14:35:57.751Z | 164.837° S | 2026-10-18 14:38:57.751Z | 203.083° SW | 23.648° | 2026-10-18 14:42:57.751Z | 252.404° 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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