METEOR M2-3 DEB, 60448

Orbit data source: Space-Track

METEOR M2-3 DEB, 60448 is space debris in SSO originally from a Commonwealth of Independent States-origin launch on Tue, 27 Jun 2023 UTC launched from the Vostochny Cosmodrome (VOSTO). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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Identifier
60448, 2023-091BC
Orbit
SSO
Country
Flag of CISCIS
Related business
Manufacturer
VNIIEM
Mission
Spacecraft
Bus & Motor
RESURS-O, Unknown motor
Mass
Unknown
Launch date (UTC)
2023-06-27 (3 years ago)
Launch vehicle
Unknown
Launch site
Vostochny Cosmodrome (VOSTO)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 METEOR M2-3 DEB
1 60448U 23091BC  26256.08203742  .00000191  00000-0  10005-3 0  9994
2 60448  98.6028 310.2938 0002779 268.3588  91.7274 14.25087570131349
Epoch: 2026-09-13T01:58Z
TLE epoch observation values (Epoch: 2026-09-13T01:58:08.033Z)
Latitude
0.00007°
Longitude
-71.32148°
Altitude
811.184 km
Speed
7.448 km/s
True Right ascension
20h 41m 10s
True Declination
0° 00' 00"
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
22:40:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
807.341 km
Perigee altitude
803.349 km
Semi-major axis
7,183.482 km
Eccentricity
0.00028
Inclination
98.6028°
RAAN
310.2938°
Arg. of periapsis
268.3588°
True anomaly
91.75923°
Mean anomaly
91.7274°
Eccentric anomaly
91.74332°
Mean motion
3.56485 °/min
Orbital period
100.99 mins
BSTAR
0.00010005
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