COSMOS 1995, 19786
Orbit data source: Space-Track
COSMOS 1995, 19786 is a payload satellite owned by UNKS (CIS) in LEO that was launched on Fri, 10 Feb 1989 UTC via a TSIKLON-3 launch vehicle from the Plesetsk Missile And Space Complex (PKMTR). 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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19786 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Defense Communications
Bus & Motor
STRELA-3, Unknown motor
Mass
225 kg wet, 225 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
1.257 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 COSMOS 1995
1 19786U 89009B 25301.64275392 .00000022 00000-0 66318-4 0 9998
2 19786 82.6251 175.6047 0002704 299.5640 88.5597 12.62226268691134Epoch: 2025-10-28T15:25Z
TLE epoch observation values (Epoch: 2025-10-28T15:25:33.938Z)
Latitude
27.94005°
Longitude
-89.09723°
Altitude
1,417.012 km
Speed
7.155 km/s
True Right ascension
11h 58m 05s
True Declination
27° 48' 36"
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
06:01:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.194 km
Perigee altitude
1,408.982 km
Semi-major axis
7,789.225 km
Eccentricity
0.00027
Inclination
82.6251°
RAAN
175.6047°
Arg. of periapsis
299.564°
True anomaly
88.59068°
Mean anomaly
88.5597°
Eccentric anomaly
88.57519°
Mean motion
3.1572 °/min
Orbital period
114.03 mins
BSTAR
0.000066318
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Other satellites on launch #9 in the year 1989 (1989-02-10 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 1995 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 | 2025-10-29 16:06:20.208Z | 173.079° S | 2025-10-29 16:13:20.208Z | 84.546° E | 43.311° | 2025-10-29 16:21:20.208Z | 12.108° NNE |
| 10 mins | 2025-10-29 18:04:20.208Z | 252.725° W | 2025-10-29 18:09:20.208Z | 297.332° NW | 21.851° | 2025-10-29 18:14:20.208Z | 338.45° N |
| 12 mins | 2025-10-30 02:08:20.208Z | 17.595° NNE | 2025-10-30 02:14:20.208Z | 70.222° E | 25.22° | 2025-10-30 02:20:20.208Z | 121.735° SE |
| 14 mins | 2025-10-30 04:03:20.208Z | 342.138° N | 2025-10-30 04:09:20.208Z | 281.041° WNW | 40.768° | 2025-10-30 04:17:20.208Z | 192.646° SSW |
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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