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
Small (<0.1 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  26105.12428905  .00000189  00000-0  99337-4 0  9995
2 60448  98.6170 162.1604 0003780   8.5500 351.5743 14.25003728109843
Epoch: 2026-04-15T02:58Z
TLE epoch observation values (Epoch: 2026-04-15T02:58:58.573Z)
Latitude
-0.00008°
Longitude
-85.87433°
Altitude
808.717 km
Speed
7.45 km/s
True Right ascension
10h 48m 38s
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
18:04:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
808.343 km
Perigee altitude
802.912 km
Semi-major axis
7,183.765 km
Eccentricity
0.00038
Inclination
98.617°
RAAN
162.1604°
Arg. of periapsis
8.55°
True anomaly
351.56795°
Mean anomaly
351.5743°
Eccentric anomaly
351.57113°
Mean motion
3.56463 °/min
Orbital period
100.99 mins
BSTAR
0.000099337
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