FALCON 9 R/B, 62484

Orbit data source: Space-Track

FALCON 9 R/B, 62484 is space debris in HEO originally from a launch on Sat, 04 Jan 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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Iframe URL

https://www.satcat.com/sats-embedded/62484?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

62484, 2025-001B

Orbit

HEO

Last TLE update

1 day 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)

2025-01-04 (6 months ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Cyl, 15.53 m

Radar Cross Section

39.980 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago

0 FALCON 9 R/B
1 62484U 25001B   25186.18447235  .00000046  00000-0  70522-3 0  9997
2 62484  25.4188 282.5114 7960595 241.6922  20.0016  1.41740389  2585

Epoch: 2025-07-05T04:25Z

TLE epoch observation values (Epoch: 2025-07-05T04:25:38.411Z)

Latitude

0.00009°

Longitude

-67.16588°

Altitude

13,493.366 km

Speed

5.311 km/s

True Right ascension

18h 50m 40s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

23.47375°

Longitude

-1.65946°

Altitude

52,458.446 km

Speed

1.282 km/s

Apparent Right ascension

23h 33m 07s

Apparent Declination

20° 07' 48"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

18:18:37

Azimuth

81.039° E

Elevation

21.274°

Doppler factor

Orbital elements

Apogee altitude

53,755.314 km

Perigee altitude

449.948 km

Semi-major axis

33,480.768 km

Eccentricity

0.79606

Inclination

25.4188°

RAAN

282.5114°

Arg. of periapsis

241.6922°

True anomaly

Unknown

Mean anomaly

20.0016°

Eccentric anomaly

Unknown

Mean motion

0.35428 °/min

Orbital period

1,016.14 mins

BSTAR

0.00070522

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Other satellites on launch #1 in the year 2025 (2025-01-04 UTC)

THURAYA 4, 62483

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.
384 mins	2025-07-06 06:21:07.736Z	81.05° E	2025-07-06 11:00:07.736Z	106.087° ESE	37.912°	2025-07-06 12:45:07.736Z	100.263° ESE

Authenticating...

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Check out FALCON 9 R/B, 62484 on other resources

View FALCON 9 R/B, 62484 on Heavens-Above

View FALCON 9 R/B, 62484 on Keep Track

View FALCON 9 R/B, 62484 on Celestrak

View FALCON 9 R/B, 62484 on Gunter's Space Page

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