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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 COSMOS 2596
1 65589U 25206A 26165.87322262 -.00000055 00000-0 00000+0 0 9990
2 65589 64.6399 314.9126 0065677 305.1606 54.2088 2.14901177 5903Epoch: 2026-06-14T20:57Z
TLE epoch observation values (Epoch: 2026-06-14T20:57:26.434Z)
Latitude
0.00004°
Longitude
97.36746°
Altitude
18,891.228 km
Speed
3.979 km/s
True Right ascension
20h 59m 34s
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
13:39:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,153.533 km
Perigee altitude
18,820.352 km
Semi-major axis
25,365.079 km
Eccentricity
0.00657
Inclination
64.6399°
RAAN
314.9126°
Arg. of periapsis
305.1606°
True anomaly
54.82221°
Mean anomaly
54.2088°
Eccentric anomaly
54.51521°
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. |
|---|---|---|---|---|---|---|---|
| 176 mins | 2026-06-16 06:31:13.354Z | 110.127° ESE | 2026-06-16 08:00:13.354Z | 63.872° ENE | 28.13° | 2026-06-16 09:27:13.354Z | 25.335° NE |
| 274 mins | 2026-06-16 19:31:13.354Z | 318.302° NNW | 2026-06-16 21:53:13.354Z | 268.137° W | 43.841° | 2026-06-17 00:05:13.354Z | 194.459° SSW |
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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