Showing default

METEOR M2-2, 44387

Orbit data source: Space-Track

METEOR M2-2, 44387 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Fri, 05 Jul 2019 UTC via a SOYUZ-2-1B launch vehicle from the Vostochny Cosmodrome (VOSTO). 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
44387, 2019-038A
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Partially operational Civil Weather
Bus & Motor
RESURS-O, Unknown motor
Mass
2,879 kg wet, ~2,600 kg dry
Launch date (UTC)
2019-07-05 (7 years ago)
Launch vehicle
SOYUZ-2-1B
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + 2 Pan, 7.0 m
Radar Cross Section
26.744 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 9 hours ago

TLE from 9 hours ago
0 METEOR M2-2
1 44387U 19038A   26125.95630041 -.00000187  00000-0 -61244-4 0  9990
2 44387  98.9136 112.6230 0002063 112.6298 247.5098 14.24353122355284
Epoch: 2026-05-05T22:57Z
TLE epoch observation values (Epoch: 2026-05-05T22:57:04.355Z)
Latitude
-0.00008°
Longitude
-95.46884°
Altitude
814.15 km
Speed
7.446 km/s
True Right ascension
07h 30m 29s
True Declination
0° 00' 00"
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
15:43:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.314 km
Perigee altitude
806.349 km
Semi-major axis
7,185.968 km
Eccentricity
0.00021
Inclination
98.9136°
RAAN
112.623°
Arg. of periapsis
112.6298°
True anomaly
247.48796°
Mean anomaly
247.5098°
Eccentric anomaly
247.49888°
Mean motion
3.563 °/min
Orbital period
101.04 mins
BSTAR
-0.000061244
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|