FALCON 9 R/B, 63103

Orbit data source: Space-Track

FALCON 9 R/B, 63103 is space debris in HEO originally from a launch on Thu, 27 Feb 2025 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

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https://www.satcat.com/sats-embedded/63103?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

63103, 2025-038E

Orbit

HEO

Last TLE update

5 months ago

Origin

SpaceX (US)

Manufacturer

SpaceX

Mission

Spacecraft

Bus & Motor

F9ST2, Unknown motor

Mass

~4,000 kg wet, ~4,000 kg dry

Launch date (UTC)

2025-02-27 (5 months ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 7.8 m

Radar Cross Section

39.980 m²

Expand to show TLE details & history

TLE from 5 months ago

0 FALCON 9 R/B
1 63103U 25038E   25058.03746186 -.00007054  00000-0  00000-0 0  9993
2 63103  28.5200 357.2438 9653600 216.4100   0.0142  0.10463308    09

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

20.39258°

Longitude

-125.27252°

Altitude

257,375.734 km

Speed

0.963 km/s

Apparent Right ascension

03h 04m 04s

Apparent Declination

19° 50' 48"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

00:35:11

Azimuth

111.16° ESE

Elevation

52.405°

Doppler factor

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

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Other satellites on launch #38 in the year 2025 (2025-02-27 UTC)

IM-2, 63099 (Decayed)

CHIMERA-1, 63100

LUNAR TRAILBLAZER, 63101

BROKKER-2 ODIN, 63102

FALCON 9 R/B 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.
522 mins	2025-07-19 11:45:33.859Z	111.164° ESE	2025-07-19 14:15:33.859Z	181.193° SSW	43.241°	2025-07-19 20:27:33.859Z	287.408° WNW
194 mins	2025-07-20 08:31:33.859Z	71.949° E	2025-07-20 11:45:33.859Z	101.302° ESE	35.904°	2025-07-20 11:45:33.859Z	101.302° ESE

Co-orbital & Co-planar RSOs

Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions

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Check out FALCON 9 R/B, 63103 on other resources

View FALCON 9 R/B, 63103 on Heavens-Above

View FALCON 9 R/B, 63103 on Keep Track

View FALCON 9 R/B, 63103 on Celestrak

View FALCON 9 R/B, 63103 on Gunter's Space Page

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