COSMOS 86, 1584
Orbit data source: Space-Track
COSMOS 86, 1584 is a payload satellite owned by OKB-10 (CIS) in LEO that was launched on Sat, 18 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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1584 intel report (Beta)
COSMOS 86 details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 18 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 18 hours ago
0 COSMOS 86
1 01584U 65073A 24355.92566056 -.00000102 00000-0 -42591-4 0 9997
2 01584 56.0563 172.5981 0211115 267.9664 260.9002 12.51905916709418Epoch: 2024-12-20T22:12Z
Definitive object data (Epoch: 2024-12-20T22:12:57.072Z)
| Latitude | 11.16219° |
| Longitude | -78.21842° |
| Altitude | 1,486.386 km |
| Speed | 7.109 km/s |
| True Right ascension | 23h 00m 00s |
| True Declination | 11° 06' 11" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -51.87438° |
| Longitude | -14.04723° |
| Altitude | 1,317.16 km |
| Speed | 7.271 km/s |
| Apparent Right ascension | 03h 06m 34s |
| Apparent Declination | -46° 18' 45" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 14:56:44 |
| Azimuth | 194.843° SSW |
| Elevation | -83.357° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,621.754 km |
| Perigee altitude | 1,290.958 km |
| Semi-major axis | 7,834.493 km |
| Eccentricity | 0.0211115 |
| Inclination | 56.0563° |
| RAAN | 172.5981° |
| Arg. of periapsis | 267.9664° |
| True anomaly | 258.52206° |
| Mean anomaly | 260.9002° |
| Eccentric anomaly | 259.71005° |
| Mean motion | 3.12987 °/min |
| BSTAR | -0.000042591 |
| Orbital period | 115.02 mins |
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Other satellites on launch #73 in the year 1965 (1965-09-18 UTC)
| COSMOS 86, 1584 |
| COSMOS 87, 1585 |
| COSMOS 88, 1586 |
| COSMOS 89, 1587 |
| COSMOS 90, 1588 |
| SL-8 R/B, 1589 |
| SL-8 DEB, 1590 |
| SL-8 DEB, 1591 |
| SL-8 DEB, 1617 |
| SL-8 DEB, 1618 |
| SL-8 DEB, 2647 |
COSMOS 86 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. |
|---|---|---|---|---|---|---|---|
| 17 mins | 2024-12-21 16:43:22.172Z | 275.95° WNW | 2024-12-21 16:52:22.172Z | 346.144° N | 30.847° | 2024-12-21 17:00:22.172Z | 44.274° NE |
| 15 mins | 2024-12-21 18:48:22.172Z | 315.096° NNW | 2024-12-21 18:55:22.172Z | 10.709° NNE | 27.513° | 2024-12-21 19:03:22.172Z | 67.905° E |
| 17 mins | 2024-12-21 20:49:22.172Z | 319.451° NNW | 2024-12-21 20:57:22.172Z | 27.556° NE | 39.651° | 2024-12-21 21:06:22.172Z | 110.809° ESE |
| 16 mins | 2024-12-21 22:50:22.172Z | 304.519° NW | 2024-12-21 22:58:22.172Z | 229.483° WSW | 38.107° | 2024-12-21 23:06:22.172Z | 164.135° S |
| 7 mins | 2024-12-22 11:46:22.172Z | 130.966° SE | 2024-12-22 11:49:22.172Z | 110.204° ESE | 14.226° | 2024-12-22 11:53:22.172Z | 83.8° E |
| 17 mins | 2024-12-22 13:40:22.172Z | 205.698° SW | 2024-12-22 13:48:22.172Z | 116.227° SE | 42.385° | 2024-12-22 13:57:22.172Z | 49.416° ENE |
| 13 mins | 2024-12-22 15:41:22.172Z | 262.055° W | 2024-12-22 15:48:22.172Z | 322.251° NNW | 36.372° | 2024-12-22 15:54:22.172Z | 30.058° NE |
Authenticating...
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