OPS 5712 (P/L 160), 2826
Orbit data source: Space-Track
OPS 5712 (P/L 160), 2826 is a payload satellite owned by NRL (US) in LEO that was launched on Wed, 31 May 1967 UTC via a THOR SLV-2 AGENA D 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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2826 intel report (Beta)
OPS 5712 (P/L 160) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 17 hours ago |
| Origin | |
| Manufacturer | NRL |
| Mission | Operational Defense Calibration |
| Bus & Motor | NRL 14"?, Unknown motor |
| Mass | 5 kg wet, 5 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Sphere, 0.51 m |
| Radar Cross Section | 0.204 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 17 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A 24355.88451059 .00012868 00000-0 23674-2 0 9997
2 02826 69.9220 278.5334 0002040 243.3798 116.7135 14.65737644986253Epoch: 2024-12-20T21:13Z
Definitive object data (Epoch: 2024-12-20T21:13:41.714Z)
| Latitude | -0.00003° |
| Longitude | -129.83404° |
| Altitude | 677.738 km |
| Speed | 7.518 km/s |
| True Right ascension | 18h 34m 08s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | 41.68392° |
| Longitude | -112.6063° |
| Altitude | 681.498 km |
| Speed | 7.519 km/s |
| Apparent Right ascension | 22h 10m 03s |
| Apparent Declination | 4° 18' 58" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 12:50:40 |
| Azimuth | 49.626° ENE |
| Elevation | -32.429° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 674.133 km |
| Perigee altitude | 671.256 km |
| Semi-major axis | 7,050.832 km |
| Eccentricity | 0.000204 |
| Inclination | 69.922° |
| RAAN | 278.5334° |
| Arg. of periapsis | 243.3798° |
| True anomaly | 116.73438° |
| Mean anomaly | 116.7135° |
| Eccentric anomaly | 116.72394° |
| Mean motion | 3.66592 °/min |
| BSTAR | 0.0023674 |
| Orbital period | 98.2 mins |
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Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
OPS 5712 (P/L 160) 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2024-12-21 20:16:38.674Z | 193.901° SSW | 2024-12-21 20:20:38.674Z | 141.272° SSE | 42.545° | 2024-12-21 20:25:38.674Z | 29.48° NE |
| 5 mins | 2024-12-22 04:54:38.674Z | 25.203° NE | 2024-12-22 04:56:38.674Z | 59.401° ENE | 19.97° | 2024-12-22 04:59:38.674Z | 101.271° ESE |
| 7 mins | 2024-12-22 06:33:38.674Z | 316.474° NNW | 2024-12-22 06:36:38.674Z | 265.974° W | 33.666° | 2024-12-22 06:40:38.674Z | 185.03° SSW |
Authenticating...
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