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FRAM-2, 63427

Orbit data source: Space-Track

FRAM-2, 63427 is a payload satellite owned by SpaceX (US) in LEO that was launched on Tue, 01 Apr 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
63427, 2025-066A
Orbit
LEO
Last TLE update
6 hours ago
Origin
Manufacturer
SpaceX
Mission
Operational spacecraft
Bus & Motor
DRAGON CM, Unknown motor
Mass
~13,055 kg wet, ~9,500 kg dry
Launch date (UTC)
2025-04-01 (4 days ago)
Launch vehicle
FALCON 9
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
RCS unknown

Expand to show TLE details & history

TLE from 6 hours ago
0 FRAM-2
1 63427U 25066A   25094.61586442  .00010044  00000-0  12939-3 0  9993
2 63427  89.6278 318.3051 0055076  81.7161 334.7354 15.56995629   547
Epoch: 2025-04-04T14:46Z
Definitive object data (Epoch: 2025-04-04T14:46:50.685Z)
Latitude
56.28235°
Longitude
-96.02328°
Altitude
372.204 km
Speed
7.711 km/s
True Right ascension
21h 15m 26s
True Declination
56° 06' 51"
Sunlit
Object was in daylight at TLE epoch
Visualization TLE readout
Latitude
69.91194°
Longitude
-95.57936°
Altitude
371.896 km
Speed
7.714 km/s
Apparent Right ascension
16h 39m 19s
Apparent Declination
23° 20' 52"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
02:53:45
Azimuth
333.865° NNW
Elevation
-22.117°
Doppler factor
1
Orbital elements
Apogee altitude
430.406 km
Perigee altitude
355.819 km
Semi-major axis
6,771.25 km
Eccentricity
0.0055076
Inclination
89.6278°
RAAN
318.3051°
Arg. of periapsis
81.7161°
True anomaly
334.46435°
Mean anomaly
334.7354°
Eccentric anomaly
334.60004°
Mean motion
3.89529 °/min
BSTAR
0.00012939
Orbital period
92.42 mins
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Other satellites on launch #66 in the year 2025 (2025-04-01 UTC)

FRAM-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.
4 mins2025-04-05 03:26:31.516Z349.201° N2025-04-05 03:28:31.516Z280.97° WNW39.698°2025-04-05 03:30:31.516Z199.898° SSW
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