Showing default

METEOR 3M, 27001

Orbit data source: Space-Track

METEOR 3M, 27001 is a Commonwealth of Independent States-origin payload satellite in SSO that was launched on Mon, 10 Dec 2001 UTC via a ZENIT-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
27001, 2001-056A
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Civil Weather
Bus & Motor
METEOR-3, Unknown motor
Mass
2,476 kg wet, ~2,300 kg dry
Launch date (UTC)
2001-12-10 (24 years ago)
Launch vehicle
ZENIT-2
Launch site
Tyuratam Missile And Space Complex (TTMTR)
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: 10 hours ago

TLE from 10 hours ago
0 METEOR 3M
1 27001U 01056A   25324.27835213 -.00000005  00000-0  48179-4 0  9998
2 27001  99.8157 141.9155 0013808  14.5490 158.2209 13.69028313196290
Epoch: 2025-11-20T06:40Z
TLE epoch observation values (Epoch: 2025-11-20T06:40:49.624Z)
Latitude
6.99541°
Longitude
163.38085°
Altitude
1,014.703 km
Speed
7.34 km/s
True Right ascension
21h 32m 30s
True Declination
6° 57' 19"
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
13:23:22
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,010.532 km
Perigee altitude
990.155 km
Semi-major axis
7,378.481 km
Eccentricity
0.00138
Inclination
99.8157°
RAAN
141.9155°
Arg. of periapsis
14.549°
True anomaly
158.27951°
Mean anomaly
158.2209°
Eccentric anomaly
158.25022°
Mean motion
3.42447 °/min
Orbital period
105.13 mins
BSTAR
0.000048179
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
|