COSMOS 82, 1572
Orbit data source: Space-Track
COSMOS 82, 1572 is a payload satellite owned by OKB-10 (CIS) in LEO that was launched on Fri, 03 Sep 1965 UTC via a KOSMOS 65S3 launch vehicle from the Tyuratam Missile And Space Complex (TTMTR). 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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1572 intel report (Beta)
COSMOS 82 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 17 hours ago |
| Origin | |
| Manufacturer | OKB-10 |
| Mission | Defense Communications |
| Bus & Motor | STRELA-1 11F610, Unknown motor |
| Mass | 50 kg wet, 50 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Poly, 0.8 m |
| Radar Cross Section | 0.731 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 17 hours ago
0 COSMOS 82
1 01572U 65070C 24355.80245928 -.00000077 00000-0 11389-3 0 9990
2 01572 56.0597 270.6805 0072524 253.4691 140.7636 12.45113309696521Epoch: 2024-12-20T19:15Z
Definitive object data (Epoch: 2024-12-20T19:15:32.481Z)
| Latitude | 28.29437° |
| Longitude | -86.93539° |
| Altitude | 1,531.013 km |
| Speed | 7.083 km/s |
| True Right ascension | 19h 27m 15s |
| True Declination | 28° 09' 54" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -7.5204° |
| Longitude | -115.0458° |
| Altitude | 1,493.53 km |
| Speed | 7.115 km/s |
| Apparent Right ascension | 19h 40m 05s |
| Apparent Declination | -28° 25' 48" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:23:45 |
| Azimuth | 93.842° ESE |
| Elevation | -43.117° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,541.85 km |
| Perigee altitude | 1,427.799 km |
| Semi-major axis | 7,862.962 km |
| Eccentricity | 0.0072524 |
| Inclination | 56.0597° |
| RAAN | 270.6805° |
| Arg. of periapsis | 253.4691° |
| True anomaly | 141.28559° |
| Mean anomaly | 140.7636° |
| Eccentric anomaly | 141.02496° |
| Mean motion | 3.11289 °/min |
| BSTAR | 0.00011389 |
| Orbital period | 115.65 mins |
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)
| COSMOS 80, 1570 |
| COSMOS 81, 1571 |
| COSMOS 82, 1572 |
| COSMOS 83, 1573 |
| COSMOS 84, 1574 |
| SL-8 R/B, 1575 |
| SL-8 DEB *, 3045 |
COSMOS 82 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 | 2024-12-21 18:19:58.226Z | 128.182° SE | 2024-12-21 18:22:58.226Z | 108.283° ESE | 12.027° | 2024-12-21 18:24:58.226Z | 95.006° ESE |
| 16 mins | 2024-12-21 20:14:58.226Z | 200.699° SSW | 2024-12-21 20:21:58.226Z | 127.217° SE | 41.128° | 2024-12-21 20:30:58.226Z | 50.59° ENE |
| 16 mins | 2024-12-21 22:15:58.226Z | 259.422° W | 2024-12-21 22:22:58.226Z | 323.781° NNW | 37.056° | 2024-12-21 22:31:58.226Z | 41.936° NE |
| 14 mins | 2024-12-22 00:19:58.226Z | 303.284° NW | 2024-12-22 00:26:58.226Z | 0.518° NNE | 26.025° | 2024-12-22 00:33:58.226Z | 52.057° ENE |
| 15 mins | 2024-12-22 02:22:58.226Z | 321.446° NNW | 2024-12-22 02:29:58.226Z | 21.257° NNE | 32.024° | 2024-12-22 02:37:58.226Z | 88.224° E |
| 17 mins | 2024-12-22 04:23:58.226Z | 313.729° NW | 2024-12-22 04:31:58.226Z | 244.225° WSW | 44.935° | 2024-12-22 04:40:58.226Z | 139.456° SSE |
| 11 mins | 2024-12-22 06:26:58.226Z | 282.691° WNW | 2024-12-22 06:31:58.226Z | 243.959° WSW | 20.777° | 2024-12-22 06:37:58.226Z | 200.33° SSW |
Authenticating...
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