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
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 2122U 66025B 26125.38359801 .00000316 00000-0 70100-4 0 9991
2 2122 144.6340 94.0009 0047590 337.4813 22.3778 13.66166532999259Epoch: 2026-05-05T09:12Z
TLE epoch observation values (Epoch: 2026-05-05T09:12:22.868Z)
Latitude
-0.00001°
Longitude
92.64641°
Altitude
979.888 km
Speed
7.38 km/s
True Right ascension
06h 16m 00s
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
05:34:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,051.526 km
Perigee altitude
981.145 km
Semi-major axis
7,394.473 km
Eccentricity
0.00476
Inclination
144.634°
RAAN
94.0009°
Arg. of periapsis
337.4813°
True anomaly
22.58657°
Mean anomaly
22.3778°
Eccentric anomaly
22.48207°
Mean motion
3.41336 °/min
Orbital period
105.47 mins
BSTAR
0.0000701
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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 | 2026-05-06 13:48:35.479Z | 108.342° ESE | 2026-05-06 13:52:35.479Z | 166.525° S | 27.532° | 2026-05-06 13:56:35.479Z | 214.139° SW |
| 10 mins | 2026-05-06 15:27:35.479Z | 99.201° ESE | 2026-05-06 15:31:35.479Z | 157.663° S | 38.486° | 2026-05-06 15:37:35.479Z | 246.034° WSW |
| 9 mins | 2026-05-06 17:07:35.479Z | 110.537° ESE | 2026-05-06 17:11:35.479Z | 181.694° SSW | 40.518° | 2026-05-06 17:16:35.479Z | 260.31° W |
| 9 mins | 2026-05-06 18:47:35.479Z | 136.739° SSE | 2026-05-06 18:51:35.479Z | 201.425° SSW | 33.276° | 2026-05-06 18:56:35.479Z | 264.549° W |
| 6 mins | 2026-05-06 20:28:35.479Z | 174.917° S | 2026-05-06 20:31:35.479Z | 210.608° SW | 18.155° | 2026-05-06 20:34:35.479Z | 245.01° WSW |
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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