OPS 1527 (OV3-1), 2150
Orbit data source: Space-Track
OPS 1527 (OV3-1), 2150 is a payload satellite owned by USAF OAR (US) in LEO that was launched on Fri, 22 Apr 1966 UTC via an SCOUT B launch vehicle from the Air Force Western Test Range (AFWTR). Payloads include a variety of satellites, spacecraft, and rockets 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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2150 intel report (Beta)
OPS 1527 (OV3-1) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 20 hours ago |
| Origin | |
| Manufacturer | Space General |
| Mission | Civil Science |
| Bus & Motor | OV3, Unknown motor |
| Mass | 69 kg wet, 69 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Oct Cyl, 0.74 m |
| Radar Cross Section | 0.613 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 20 hours ago
0 OPS 1527 (OV3-1)
1 02150U 66034A 24364.85019121 .00034389 00000-0 18943-2 0 9997
2 02150 82.3677 177.2804 1462139 184.9526 173.5623 12.46239686334850Epoch: 2024-12-29T20:24Z
Definitive object data (Epoch: 2024-12-29T20:24:16.52Z)
| Latitude | 0.00001° |
| Longitude | 132.43095° |
| Altitude | 2,626.712 km |
| Speed | 6.151 km/s |
| True Right ascension | 11h 49m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 37.71192° |
| Longitude | -54.03928° |
| Altitude | 553.565 km |
| Speed | 8.026 km/s |
| Apparent Right ascension | 01h 36m 06s |
| Apparent Declination | 1° 00' 07" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 16:07:35 |
| Azimuth | 49.738° ENE |
| Elevation | -36.451° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 2,626.134 km |
| Perigee altitude | 328.92 km |
| Semi-major axis | 7,855.664 km |
| Eccentricity | 0.1462139 |
| Inclination | 82.3677° |
| RAAN | 177.2804° |
| Arg. of periapsis | 184.9526° |
| True anomaly | 175.15064° |
| Mean anomaly | 173.5623° |
| Eccentric anomaly | 174.38236° |
| Mean motion | 3.11723 °/min |
| BSTAR | 0.0018943 |
| Orbital period | 115.49 mins |
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Other satellites on launch #34 in the year 1966 (1966-04-22 UTC)
| OPS 1527 (OV3-1), 2150 |
| SCOUT B R/B, 2167 (Decayed) |
| SCOUT B DEB, 2208 (Decayed) |
| SCOUT B DEB, 2209 (Decayed) |
OPS 1527 (OV3-1) Visibility forecast
Observer location: undefined°, undefined
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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2024-12-31 00:08:38.326Z | 330.18° NNW | 2024-12-31 00:11:38.326Z | 263.249° W | 30.82° | 2024-12-31 00:13:38.326Z | 212.17° SW |
| 21 mins | 2024-12-31 11:01:38.326Z | 147.133° SSE | 2024-12-31 11:12:38.326Z | 91.699° ESE | 34.155° | 2024-12-31 11:22:38.326Z | 24.138° NE |
| 23 mins | 2024-12-31 12:56:38.326Z | 202.927° SW | 2024-12-31 13:09:38.326Z | 284.466° WNW | 41.568° | 2024-12-31 13:19:38.326Z | 359.805° N |
| 11 mins | 2024-12-31 15:01:38.326Z | 269.615° W | 2024-12-31 15:07:38.326Z | 298.209° NW | 15.446° | 2024-12-31 15:12:38.326Z | 325.996° NNW |
Authenticating...
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