COSMOS 1988 (GLONASS), 19750
Orbit data source: Space-Track
COSMOS 1988 (GLONASS), 19750 is a payload satellite owned by UNKS (CIS) in MEO that was launched on Tue, 10 Jan 1989 UTC via a PROTON-K/DM-2 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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19750 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Omsk Av. Zav.
Mission
Non-operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,300 kg wet, ~1,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 2 Pan, 4.2 m
Radar Cross Section
14.707 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 days ago
TLE from 6 days ago
0 COSMOS 1988 (GLONASS)
1 19750U 89001B 26068.05643853 .00000007 00000-0 00000-0 0 9993
2 19750 64.8884 76.0526 0015550 224.1403 133.4016 2.13101815289144Epoch: 2026-03-09T01:21Z
TLE epoch observation values (Epoch: 2026-03-09T01:21:16.288Z)
Latitude
-2.13858°
Longitude
-112.02952°
Altitude
19,158.011 km
Speed
3.949 km/s
True Right ascension
05h 00m 10s
True Declination
-2° 08' 06"
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
16:02:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,169.185 km
Perigee altitude
19,089.857 km
Semi-major axis
25,507.658 km
Eccentricity
0.00156
Inclination
64.8884°
RAAN
76.0526°
Arg. of periapsis
224.1403°
True anomaly
133.53089°
Mean anomaly
133.4016°
Eccentric anomaly
133.46626°
Mean motion
0.53277 °/min
Orbital period
675.72 mins
BSTAR
0
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Other satellites on launch #1 in the year 1989 (1989-01-10 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 1988 (GLONASS) 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. |
|---|---|---|---|---|---|---|---|
| 357 mins | 2026-03-16 01:39:10.289Z | 208.481° SW | 2026-03-16 04:10:10.289Z | 310.424° NW | 42.418° | 2026-03-16 07:36:10.289Z | 95.526° ESE |
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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