DECAYED
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IM-2, 63099 (Decayed)

Orbit data source: Space-Track

IM-2, 63099 was a payload satellite owned by Intuitive Mach. (US) in HEO that was launched on Thu, 27 Feb 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). 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.

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Identifier
63099, 2025-038A
Orbit
Decayed
Country
Flag of USUS
Related business
Manufacturer
Intuitive Mach.
Mission
Decayed Commercial Planetary
Bus & Motor
NOVA-C, AOCS
Mass
2,120 kg wet, ~650 kg dry
Launch date (UTC)
2025-02-27 (1 year ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 6 Leg, 2.0 m
Radar Cross Section
8.160 m²

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

TLE from 1 year ago
0 IM-2
1 63099U 25038A   25058.03746186 -.00007054  00000-0  00000-0 0  9997
2 63099  28.5200 357.2438 9653600 216.4100   0.0142  0.10463308    03
Epoch: 2025-02-27T00:53Z
TLE epoch observation values (Epoch: 2025-02-27T00:53:56.704Z)
Latitude
-2.41715°
Longitude
-177.27109°
Altitude
51,153.232 km
Speed
3.429 km/s
True Right ascension
23h 33m 20s
True Declination
-2° 24' 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
12:14:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
367,518.128 km
Perigee altitude
211.885 km
Semi-major axis
190,243.144 km
Eccentricity
0.96536
Inclination
28.52°
RAAN
357.2438°
Arg. of periapsis
216.41°
True anomaly
3.0537°
Mean anomaly
0.0142°
Eccentric anomaly
0.4055°
Mean motion
0.02616 °/min
Orbital period
13,763.31 mins
BSTAR
0
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Other satellites on launch #38 in the year 2025 (2025-02-27 UTC)

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