Showing default

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.

Loading next visibility...
Identifier
28917, 2005-050C
Orbit
MEO
Country
Flag of CISCIS
Related 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)
2005-12-25 (20 years ago)
Launch vehicle
PROTON-K/DM-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 1 Arm + 2 Pan, 3.9 m
Radar Cross Section
8.145 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 COSMOS 2417 (GLONASS)
1 28917U 05050C   26041.11155742 -.00000077  00000-0  00000-0 0  9991
2 28917  65.6437 320.4163 0015359  95.9203  61.0738  2.13104194156529
Epoch: 2026-02-10T02:40Z
TLE epoch observation values (Epoch: 2026-02-10T02:40:38.561Z)
Latitude
20.72962°
Longitude
-49.78504°
Altitude
19,111.299 km
Speed
3.956 km/s
True Right ascension
08h 42m 17s
True Declination
20° 41' 52"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:18:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,168.482 km
Perigee altitude
19,090.128 km
Semi-major axis
25,507.442 km
Eccentricity
0.00154
Inclination
65.6437°
RAAN
320.4163°
Arg. of periapsis
95.9203°
True anomaly
61.22799°
Mean anomaly
61.0738°
Eccentric anomaly
61.15088°
Mean motion
0.53277 °/min
Orbital period
675.71 mins
BSTAR
0
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|