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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OPS 5712 (P/L 160) details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 10 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 10 hours ago
0 OPS 5712 (P/L 160)
1 02826U 67053A 24284.57672768 .00025543 00000-0 49771-2 0 9996
2 02826 69.9225 89.6334 0005067 246.4355 113.6253 14.62939327975810Epoch: 2024-10-10T13:50Z
Definitive object data (Epoch: 2024-10-10T13:50:29.271Z)
| Latitude | -0.00005° |
| Longitude | -137.64787° |
| Altitude | 687.515 km |
| Speed | 7.512 km/s |
| True Right ascension | 05h 58m 32s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | -24.5643° |
| Longitude | -148.18242° |
| Altitude | 692.127 km |
| Speed | 7.509 km/s |
| Apparent Right ascension | 05h 32m 34s |
| Apparent Declination | -31° 45' 54" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 17:53:50 |
| Azimuth | 29.469° NE |
| Elevation | -80.784° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 685.265 km |
| Perigee | 678.111 km |
| Semi-major axis | 7,059.825 km |
| Eccentricity | 0.0005067 |
| Inclination | 69.9225° |
| RAAN | 89.6334° |
| Arg. of periapsis | 246.4355° |
| True anomaly | 113.67848° |
| Mean anomaly | 113.6253° |
| Eccentric anomaly | 113.65189° |
| Mean motion | 3.65891 °/min |
| BSTAR | 0.0049771 |
| Period | 98.39 mins |
No data available
No data available
Other satellites on launch #53 in the year 1967 (1967-05-31 UTC)
OPS 5712 (P/L 160) Visibility forecast
Observer location: 39.9160978°, -105.1181434
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. |
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