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

3 days 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 3 days ago

0 FALCON 9 R/B
1 62484U 25001B   25193.94201593 -.00000019  00000-0  53665-3 0  9994
2 62484  25.3836 280.7846 7959472 244.4970  18.3909  1.41741227  2697

Epoch: 2025-07-12T22:36Z

TLE epoch observation values (Epoch: 2025-07-12T22:36:30.176Z)

Latitude

0.00118°

Longitude

10.84237°

Altitude

12,474.674 km

Speed

5.511 km/s

True Right ascension

18h 44m 09s

True Declination

0° 00' 04"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

15.6802°

Longitude

46.33158°

Altitude

36,510.408 km

Speed

2.585 km/s

Apparent Right ascension

21h 07m 05s

Apparent Declination

9° 14' 04"

Sunlit

Object is in daylight

Visualization observer readout

Local Sidereal Time

09:15:18

Azimuth

2.677° NNE

Elevation

-40.813°

Doppler factor

Orbital elements

Apogee altitude

53,751.319 km

Perigee altitude

453.681 km

Semi-major axis

33,480.637 km

Eccentricity

0.79595

Inclination

25.3836°

RAAN

280.7846°

Arg. of periapsis

244.497°

True anomaly

Unknown

Mean anomaly

18.3909°

Eccentric anomaly

Unknown

Mean motion

0.35428 °/min

Orbital period

1,016.13 mins

BSTAR

0.00053665

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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.
218 mins	2025-07-16 05:32:58.641Z	71.263° E	2025-07-16 07:55:58.641Z	80.781° E	19.203°	2025-07-16 09:10:58.641Z	81.822° E
105 mins	2025-07-16 12:16:58.641Z	265.611° W	2025-07-16 13:00:58.641Z	270.22° WNW	12.172°	2025-07-16 14:01:58.641Z	277.173° WNW

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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.