COSMOS 80, 1570
Orbit data source: Space-Track
COSMOS 80, 1570 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). Payload-class satellites include a variety of spacecraft 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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1570 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
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
Shape & HBR
Poly, 0.4 m
Radar Cross Section
0.731 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 COSMOS 80
1 01570U 65070A 25257.43078503 -.00000102 00000-0 -35378-4 0 9997
2 01570 56.0554 138.7960 0099478 309.0011 223.9094 12.52795480746790Epoch: 2025-09-14T10:20Z
TLE epoch observation values (Epoch: 2025-09-14T10:20:19.826Z)
Latitude
6.48515°
Longitude
165.69674°
Altitude
1,509.767 km
Speed
7.085 km/s
True Right ascension
20h 57m 43s
True Declination
6° 27' 01"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
23:03:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,530.546 km
Perigee altitude
1,374.748 km
Semi-major axis
7,830.784 km
Eccentricity
0.00995
Inclination
56.0554°
RAAN
138.796°
Arg. of periapsis
309.0011°
True anomaly
223.12588°
Mean anomaly
223.9094°
Eccentric anomaly
223.51694°
Mean motion
3.1321 °/min
Orbital period
114.94 mins
BSTAR
-0.000035378
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Other satellites on launch #70 in the year 1965 (1965-09-03 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.COSMOS 80 Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-15 16:10:49.959Z | 140.477° SSE | 2025-09-15 16:14:49.959Z | 110.918° ESE | 15.435° | 2025-09-15 16:18:49.959Z | 82.299° E |
| 16 mins | 2025-09-15 18:05:49.959Z | 211.032° SW | 2025-09-15 18:13:49.959Z | 107.486° ESE | 43.378° | 2025-09-15 18:21:49.959Z | 48.696° ENE |
| 15 mins | 2025-09-15 20:06:49.959Z | 266.022° W | 2025-09-15 20:13:49.959Z | 327.794° NNW | 34.154° | 2025-09-15 20:21:49.959Z | 39.741° NE |
| 13 mins | 2025-09-15 22:10:49.959Z | 310.366° NW | 2025-09-15 22:16:49.959Z | 0.44° NNE | 25.566° | 2025-09-15 22:23:49.959Z | 54.24° ENE |
| 15 mins | 2025-09-16 00:12:49.959Z | 324.312° NNW | 2025-09-16 00:19:49.959Z | 32.543° NE | 33.94° | 2025-09-16 00:27:49.959Z | 95.59° ESE |
| 16 mins | 2025-09-16 02:12:49.959Z | 311.13° NW | 2025-09-16 02:20:49.959Z | 203.658° SW | 43.892° | 2025-09-16 02:28:49.959Z | 146.494° SSE |
| 10 mins | 2025-09-16 04:14:49.959Z | 278.642° WNW | 2025-09-16 04:18:49.959Z | 250.22° W | 17.404° | 2025-09-16 04:24:49.959Z | 208.501° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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