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CHIMERA-1, 63100

Orbit data source: Space-Track

CHIMERA-1, 63100 is an American payload satellite 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
63100, 2025-038B
Orbit
HEO
Last TLE update
5 months ago
Origin
Manufacturer
EPICA
Mission
Operational N Technology
Bus & Motor
CHIMERA, AOCS
Mass
301 kg wet, ~150 kg dry
Launch date (UTC)
2025-02-27 (5 months ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Box, 0.6 m
Radar Cross Section
1.085 m²

Expand to show TLE details & history

TLE from 5 months ago
0 CHIMERA-1
1 63100U 25038B   25058.03746186 -.00007054  00000-0  00000+0 0  9999
2 63100  28.5200 357.2438 9653600 216.4100   0.0142  0.10463308    06
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
20.39992°
Longitude
-125.23683°
Altitude
256,912.705 km
Speed
0.966 km/s
Apparent Right ascension
03h 04m 05s
Apparent Declination
19° 51' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
00:43:45
Azimuth
113.343° SE
Elevation
53.932°
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
Orbital period
13,763.31 mins
BSTAR
0
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