COSMOS 2596, 65589
Orbit data source: Space-Track
COSMOS 2596, 65589 is a payload satellite owned by Mozhaiskiy (CIS) in MEO that was launched on Sat, 13 Sep 2025 UTC via a SOYUZ-2-1B 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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65589 intel report (Beta)
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Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Operational Civil Technology
Bus & Motor
CUBESAT?, Unknown motor
Mass
~20 kg wet, ~20 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Poly, 14.5 m
Radar Cross Section
1.143 m²
Expand to show TLE details & historyLast TLE update: 17 hours ago
TLE from 17 hours ago
0 COSMOS 2596
1 65589U 25206A 26117.94407961 -.00000037 00000-0 00000-0 0 9996
2 65589 64.6675 316.6122 0066097 305.6578 53.7562 2.14901281 4877Epoch: 2026-04-27T22:39Z
TLE epoch observation values (Epoch: 2026-04-27T22:39:28.478Z)
Latitude
0°
Longitude
120.82751°
Altitude
18,889.765 km
Speed
3.98 km/s
True Right ascension
21h 06m 29s
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
23:35:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,154.589 km
Perigee altitude
18,819.278 km
Semi-major axis
25,365.07 km
Eccentricity
0.00661
Inclination
64.6675°
RAAN
316.6122°
Arg. of periapsis
305.6578°
True anomaly
54.37005°
Mean anomaly
53.7562°
Eccentric anomaly
54.06283°
Mean motion
0.53727 °/min
Orbital period
670.06 mins
BSTAR
0
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Other satellites on launch #206 in the year 2025 (2025-09-13 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 2596 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. |
|---|---|---|---|---|---|---|---|
| 274 mins | 2026-04-28 22:52:12.194Z | 318.324° NNW | 2026-04-29 01:15:12.194Z | 268.295° W | 43.761° | 2026-04-29 03:26:12.194Z | 195.122° SSW |
| 92 mins | 2026-04-29 09:14:12.194Z | 69.176° E | 2026-04-29 10:00:12.194Z | 46.348° ENE | 15.298° | 2026-04-29 10:46:12.194Z | 24.927° NE |
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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