COSMOS 88, 1586
Orbit data source: Space-Track
COSMOS 88, 1586 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). 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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1586 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
POLY, 1.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 COSMOS 88
1 01586U 65073C 26302.68857399 -.00000081 00000-0 83376-4 0 9990
2 01586 56.0631 23.9594 0187356 347.7499 168.3359 12.43346989775225Epoch: 2026-10-29T16:31Z
TLE epoch observation values (Epoch: 2026-10-29T16:31:32.792Z)
Latitude
19.33832°
Longitude
-95.53953°
Altitude
1,637.587 km
Speed
6.99 km/s
True Right ascension
12h 41m 27s
True Declination
19° 14' 34"
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
22:23:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,639.726 km
Perigee altitude
1,344.813 km
Semi-major axis
7,870.407 km
Eccentricity
0.01874
Inclination
56.0631°
RAAN
23.9594°
Arg. of periapsis
347.7499°
True anomaly
168.76021°
Mean anomaly
168.3359°
Eccentric anomaly
168.54902°
Mean motion
3.10848 °/min
Orbital period
115.81 mins
BSTAR
0.000083376
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Other satellites on launch #73 in the year 1965 (1965-09-18 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 88 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. |
|---|---|---|---|---|---|---|---|
| 16 mins | 2026-10-30 07:13:18.115Z | 200.023° SSW | 2026-10-30 07:21:18.115Z | 125.72° SE | 54.593° | 2026-10-30 07:29:18.115Z | 52.694° ENE |
| 15 mins | 2026-10-30 09:15:18.115Z | 256.274° W | 2026-10-30 09:22:18.115Z | 324.443° NNW | 50.066° | 2026-10-30 09:30:18.115Z | 39.877° NE |
| 14 mins | 2026-10-30 11:19:18.115Z | 301.812° NW | 2026-10-30 11:25:18.115Z | 350.012° N | 28.898° | 2026-10-30 11:33:18.115Z | 51.14° ENE |
| 16 mins | 2026-10-30 13:22:18.115Z | 320.843° NNW | 2026-10-30 13:29:18.115Z | 19.106° NNE | 37.705° | 2026-10-30 13:38:18.115Z | 88.245° E |
| 17 mins | 2026-10-30 15:24:18.115Z | 315.004° NNW | 2026-10-30 15:32:18.115Z | 124.041° SE | 83.291° | 2026-10-30 15:41:18.115Z | 136.501° SSE |
| 13 mins | 2026-10-30 17:26:18.115Z | 287.421° WNW | 2026-10-30 17:32:18.115Z | 241.737° WSW | 26.335° | 2026-10-30 17:39:18.115Z | 193.744° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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