COSMOS 2532, 43753
Orbit data source: Space-Track
COSMOS 2532, 43753 is a payload satellite owned by VVKO VKS (CIS) in LEO that was launched on Fri, 30 Nov 2018 UTC via an ROKOT 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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43753 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
Resehetnev ISS
Mission
Operational Defense Communications
Bus & Motor
STRELA-3M, Unknown motor
Mass
280 kg wet, 280 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Ant, 3.5 m
Radar Cross Section
1.583 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 COSMOS 2532
1 43753U 18097C 26305.83310299 -.00000065 00000-0 -54414-3 0 9992
2 43753 82.5108 136.7060 0018402 115.1502 245.1489 12.42913111359376Epoch: 2026-11-01T19:59Z
TLE epoch observation values (Epoch: 2026-11-01T19:59:40.098Z)
Latitude
-0.00001°
Longitude
155.67012°
Altitude
1,503.09 km
Speed
7.11 km/s
True Right ascension
09h 06m 49s
True Declination
0° 00' 00"
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
20:08:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,506.111 km
Perigee altitude
1,477.147 km
Semi-major axis
7,869.766 km
Eccentricity
0.00184
Inclination
82.5108°
RAAN
136.706°
Arg. of periapsis
115.1502°
True anomaly
244.95774°
Mean anomaly
245.1489°
Eccentric anomaly
245.0533°
Mean motion
3.10885 °/min
Orbital period
115.8 mins
BSTAR
-0.00054414
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Other satellites on launch #97 in the year 2018 (2018-11-30 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 2532 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 | 2026-11-02 00:28:04.777Z | 357.057° N | 2026-11-02 00:36:04.777Z | 75.154° E | 70.299° | 2026-11-02 00:44:04.777Z | 163.142° S |
| 11 mins | 2026-11-02 02:27:04.777Z | 320.364° NNW | 2026-11-02 02:32:04.777Z | 279.748° WNW | 23.549° | 2026-11-02 02:38:04.777Z | 233.3° WSW |
| 7 mins | 2026-11-02 11:37:04.777Z | 100.278° ESE | 2026-11-02 11:40:04.777Z | 78.578° E | 14.848° | 2026-11-02 11:44:04.777Z | 49.593° ENE |
| 16 mins | 2026-11-02 13:28:04.777Z | 180.78° SSW | 2026-11-02 13:36:04.777Z | 61.316° ENE | 81.074° | 2026-11-02 13:44:04.777Z | 9.557° NNE |
| 10 mins | 2026-11-02 15:29:04.777Z | 259.222° W | 2026-11-02 15:34:04.777Z | 299.53° NW | 20.578° | 2026-11-02 15:39:04.777Z | 337.312° NNW |
| 14 mins | 2026-11-02 23:40:04.777Z | 11.686° NNE | 2026-11-02 23:46:04.777Z | 66.345° ENE | 39.112° | 2026-11-02 23:54:04.777Z | 138.574° SSE |
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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