COSMOS 1348, 13124
Orbit data source: Space-Track
COSMOS 1348, 13124 is a payload satellite owned by PVO (CIS) in HEO that was launched on Wed, 07 Apr 1982 UTC via an MOLNIYA 8K78M 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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13124 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
NPOL/KOMET
Mission
Spacecraft
Bus & Motor
OKO, Unknown motor
Mass
~1,250 kg wet, ~1,150 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 3 days ago
TLE from 3 days ago
0 COSMOS 1348
1 13124U 82029A 26170.90947455 .00000090 00000-0 00000-0 0 9990
2 13124 71.8081 145.4208 4850061 332.2556 134.6078 2.00395236323447Epoch: 2026-06-19T21:49Z
TLE epoch observation values (Epoch: 2026-06-19T21:49:38.601Z)
Latitude
43.39472°
Longitude
71.77845°
Altitude
31,264.133 km
Speed
2.487 km/s
True Right ascension
20h 29m 17s
True Declination
43° 21' 44"
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
23:20:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
33,084.953 km
Perigee altitude
7,307.498 km
Semi-major axis
26,574.362 km
Eccentricity
0.48501
Inclination
71.8081°
RAAN
145.4208°
Arg. of periapsis
332.2556°
True anomaly
161.41441°
Mean anomaly
134.6078°
Eccentric anomaly
148.94355°
Mean motion
0.50101 °/min
Orbital period
718.54 mins
BSTAR
0
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Other satellites on launch #29 in the year 1982 (1982-04-07 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 1348 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. |
|---|---|---|---|---|---|---|---|
| 111 mins | 2026-06-22 12:17:50.047Z | 233.163° WSW | 2026-06-22 12:17:50.047Z | 233.163° WSW | 36.171° | 2026-06-22 14:08:50.047Z | 232.419° WSW |
| 67 mins | 2026-06-22 18:13:50.047Z | 48.996° ENE | 2026-06-22 18:40:50.047Z | 28.186° NE | 13.611° | 2026-06-22 19:20:50.047Z | 10.25° NNE |
| 362 mins | 2026-06-23 06:15:50.047Z | 314.267° NW | 2026-06-23 09:48:50.047Z | 295.139° NW | 44.875° | 2026-06-23 12:17:50.047Z | 233.64° WSW |
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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