COSMOS 2417 (GLONASS), 28917
Orbit data source: Space-Track
COSMOS 2417 (GLONASS), 28917 is a Commonwealth of Independent States-origin payload satellite in MEO that was launched on Sun, 25 Dec 2005 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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28917 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
NPO PM
Mission
Non-operational Defense Navigation
Bus & Motor
URAGAN, Unknown motor
Mass
1,450 kg wet, ~1,200 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Cyl + 1 Arm + 2 Pan, 3.9 m
Radar Cross Section
8.145 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 COSMOS 2417 (GLONASS)
1 28917U 05050C 25306.65511227 -.00000008 00000-0 00000+0 0 9990
2 28917 65.6989 323.7582 0013483 103.2445 73.9513 2.13103856154401Epoch: 2025-11-02T15:43Z
TLE epoch observation values (Epoch: 2025-11-02T15:43:21.700Z)
Latitude
2.41803°
Longitude
-135.32964°
Altitude
19,120.607 km
Speed
3.955 km/s
True Right ascension
09h 30m 42s
True Declination
2° 24' 50"
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
20:40:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,163.722 km
Perigee altitude
19,094.939 km
Semi-major axis
25,507.467 km
Eccentricity
0.00135
Inclination
65.6989°
RAAN
323.7582°
Arg. of periapsis
103.2445°
True anomaly
74.09985°
Mean anomaly
73.9513°
Eccentric anomaly
74.02557°
Mean motion
0.53277 °/min
Orbital period
675.71 mins
BSTAR
0
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Other satellites on launch #50 in the year 2005 (2005-12-25 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 2417 (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. |
|---|---|---|---|---|---|---|---|
| 338 mins | 2025-11-15 01:27:37.536Z | 199.219° SSW | 2025-11-15 03:52:37.536Z | 300.283° NW | 43.577° | 2025-11-15 07:05:37.536Z | 79.854° E |
| 23 mins | 2025-11-15 16:54:37.536Z | 329.098° NNW | 2025-11-15 17:05:37.536Z | 323.798° NNW | 10.374° | 2025-11-15 17:17:37.536Z | 317.957° NNW |
| 8 mins | 2025-11-15 23:55:37.536Z | 177.897° S | 2025-11-16 00:03:37.536Z | 177.695° S | 14.523° | 2025-11-16 00:03:37.536Z | 177.695° S |
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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