COSMOS 2419 (GLONASS), 28915
Orbit data source: Space-Track
COSMOS 2419 (GLONASS), 28915 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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28915 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CISRelated business
Manufacturer
Polyot
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 + 2 Pan, 4.2 m
Radar Cross Section
14.707 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 COSMOS 2419 (GLONASS)
1 28915U 05050A 25259.58639191 -.00000059 00000-0 00000-0 0 9995
2 28915 65.7195 325.3078 0014109 329.6737 11.3427 2.13108238153533Epoch: 2025-09-16T14:04Z
TLE epoch observation values (Epoch: 2025-09-16T14:04:24.261Z)
Latitude
-17.30557°
Longitude
110.37907°
Altitude
19,098.698 km
Speed
3.958 km/s
True Right ascension
21h 09m 01s
True Declination
-17° 16' 42"
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
20:42:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,164.968 km
Perigee altitude
19,092.992 km
Semi-major axis
25,507.117 km
Eccentricity
0.00141
Inclination
65.7195°
RAAN
325.3078°
Arg. of periapsis
329.6737°
True anomaly
11.37455°
Mean anomaly
11.3427°
Eccentric anomaly
11.35862°
Mean motion
0.53278 °/min
Orbital period
675.7 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 2419 (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. |
|---|---|---|---|---|---|---|---|
| 285 mins | 2025-09-18 13:27:31.826Z | 314.455° NW | 2025-09-18 15:59:31.826Z | 262.121° W | 44.654° | 2025-09-18 18:12:31.826Z | 188.639° SSW |
| 72 mins | 2025-09-19 00:19:31.826Z | 59.23° ENE | 2025-09-19 00:55:31.826Z | 41.484° NE | 13.441° | 2025-09-19 01:31:31.826Z | 24.444° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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