Showing default

COSMOS 2418 (GLONASS), 28916

Orbit data source: Space-Track

COSMOS 2418 (GLONASS), 28916 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
28916, 2005-050B
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 (21 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: 23 hours ago

TLE from 23 hours ago
0 COSMOS 2418 (GLONASS)
1 28916U 05050B   26313.19330663 -.00000049  00000-0  00000-0 0  9996
2 28916  65.5055 311.3920 0013914 277.8375  99.3186  2.13106246162358
Epoch: 2026-11-09T04:38Z
TLE epoch observation values (Epoch: 2026-11-09T04:38:21.692Z)
Latitude
15.72365°
Longitude
-159.20559°
Altitude
19,135.45 km
Speed
3.952 km/s
True Right ascension
21h 15m 01s
True Declination
15° 41' 55"
Sunlit
Object was in daylight 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
23:33:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
19,164.637 km
Perigee altitude
19,093.655 km
Semi-major axis
25,507.283 km
Eccentricity
0.00139
Inclination
65.5055°
RAAN
311.392°
Arg. of periapsis
277.8375°
True anomaly
99.47589°
Mean anomaly
99.3186°
Eccentric anomaly
99.39725°
Mean motion
0.53278 °/min
Orbital period
675.7 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
|