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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Identifier
Orbit
Country
CISRelated business
Manufacturer
OKB-10
Mission
Spacecraft
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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 COSMOS 80
1 1570U 65070A 26195.97458124 -.00000094 00000-0 16495-4 0 9997
2 1570 56.0569 35.2066 0100862 0.8431 148.3194 12.52800817784835Epoch: 2026-07-14T23:23Z
TLE epoch observation values (Epoch: 2026-07-14T23:23:23.819Z)
Latitude
24.74759°
Longitude
-86.46312°
Altitude
1,521.412 km
Speed
7.077 km/s
True Right ascension
13h 08m 53s
True Declination
24° 37' 47"
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
05:31:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,531.607 km
Perigee altitude
1,373.642 km
Semi-major axis
7,830.762 km
Eccentricity
0.01009
Inclination
56.0569°
RAAN
35.2066°
Arg. of periapsis
0.8431°
True anomaly
148.91995°
Mean anomaly
148.3194°
Eccentric anomaly
148.62031°
Mean motion
3.13211 °/min
Orbital period
114.94 mins
BSTAR
0.000016495
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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. |
|---|---|---|---|---|---|---|---|
| 15 mins | 2026-07-15 17:59:57.894Z | 277.043° WNW | 2026-07-15 18:07:57.894Z | 345.628° N | 29.24° | 2026-07-15 18:14:57.894Z | 41.607° NE |
| 12 mins | 2026-07-15 20:04:57.894Z | 320.687° NNW | 2026-07-15 20:09:57.894Z | 4.171° NNE | 25.514° | 2026-07-15 20:16:57.894Z | 61.553° ENE |
| 16 mins | 2026-07-15 22:04:57.894Z | 320.785° NNW | 2026-07-15 22:12:57.894Z | 43.833° NE | 38.424° | 2026-07-15 22:20:57.894Z | 108.982° ESE |
| 15 mins | 2026-07-16 00:05:57.894Z | 303.381° NW | 2026-07-16 00:12:57.894Z | 230.158° WSW | 38.719° | 2026-07-16 00:20:57.894Z | 162.303° S |
| 15 mins | 2026-07-16 14:55:57.894Z | 203.872° SW | 2026-07-16 15:02:57.894Z | 135.26° SSE | 41.277° | 2026-07-16 15:10:57.894Z | 51.387° ENE |
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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