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IM-2, 63099

Orbit data source: Space-Track

IM-2, 63099 is 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
HEO
Last TLE update
2 months ago
Origin
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 (2 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box + 6 Leg, 4.6 m
Radar Cross Section
8.160 m²

Expand to show TLE details & history

TLE from 2 months 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
Definitive object data (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 TLE epoch
Visualization TLE readout
Latitude
20.75756°
Longitude
-128.83175°
Altitude
212,063.29 km
Speed
1.247 km/s
Apparent Right ascension
02h 51m 52s
Apparent Declination
19° 32' 21"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
18:53:28
Azimuth
55.882° ENE
Elevation
-8.187°
Doppler factor
1
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
BSTAR
Unknown
Orbital period
13763.31 mins
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Other satellites on launch #38 in the year 2025 (2025-02-27 UTC)

IM-2 Visibility forecast

Observer location: undefined°, undefined°

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Start Az.
Max El. time (UTC)
Max El. Az.
Max El.
End time (UTC)
End Az.
752 mins2025-04-24 13:30:55.100Z72.617° E2025-04-24 19:45:55.100Z180.805° SSW43.378°2025-04-25 02:02:55.100Z288.559° WNW
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