DECAYED

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FRAM-2, 63427 (Decayed)

Orbit data source: Space-Track

FRAM-2, 63427 was 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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<iframe src="https://www.satcat.com/sats-embedded/63427?theme=dark&initialShowStats=false" width="600" height="400" frameborder="0" title="Kayhan Space Satcat Satellite Viewer"></iframe>

Iframe URL

https://www.satcat.com/sats-embedded/63427?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63427, 2025-066A

Orbit

Decayed

Last TLE update

1 month ago

Origin

SpaceX (US)

Manufacturer

SpaceX

Mission

Decayed spacecraft

Bus & Motor

DRAGON CM, Unknown motor

Mass

~13,055 kg wet, ~9,500 kg dry

Launch date (UTC)

2025-04-01 (1 month 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

Large (>1 m²)

Expand to show TLE details & history

TLE from 1 month ago

0 FRAM-2
1 63427U 25066A   25094.61586442  .00010823  00000-0  12937-3 0  9996
2 63427  89.6759 318.3003 0074001  97.4684 319.2422 15.57450931   548

Epoch: 2025-04-04T14:46Z

Definitive object data (Epoch: 2025-04-04T14:46:50.685Z)

Latitude

56.25553°

Longitude

-96.10025°

Altitude

366.775 km

Speed

7.716 km/s

True Right ascension

21h 15m 07s

True Declination

56° 05' 14"

Sunlit

Object was in daylight at TLE epoch

Visualization observer readout

No trajectory is available.

Visualization observer readout

No trajectory is available.

Orbital elements

Apogee altitude

441.89 km

Perigee altitude

341.693 km

Semi-major axis

6,769.929 km

Eccentricity

0.0074001

Inclination

89.6759°

RAAN

318.3003°

Arg. of periapsis

97.4684°

True anomaly

318.68468°

Mean anomaly

319.2422°

Eccentric anomaly

318.96383°

Mean motion

3.89643 °/min

BSTAR

0.00012937

Orbital period

92.39 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°

Span	Click to sort rows by Start time (UTC) header in descending order	Start Az.	Max El. time (UTC)	Max El. Az.	Max El.	End time (UTC)	End Az.
4 mins	2025-05-02 13:21:07.643Z	171.326° S	2025-05-02 13:23:07.643Z	65.122° ENE	44.131°	2025-05-02 13:25:07.643Z	2.389° NNE

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Check out FRAM-2, 63427 (Decayed) on other resources

View FRAM-2, 63427 (Decayed) on Celestrak

View FRAM-2, 63427 (Decayed) on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.