FALCON 9 R/B, 61184

Orbit data source: Space-Track

FALCON 9 R/B, 61184 is space debris originally from a launch on Tue, 17 Sep 2024 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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Identifier
61184, 2024-167C
Orbit
Active
Country
Flag of USUS
Related business
Manufacturer
SpaceX
Mission
Spacecraft
Bus & Motor
F9ST2, Unknown motor
Mass
~4,000 kg wet, ~4,000 kg dry
Launch date (UTC)
2024-09-17 (2 years 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, Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 2 weeks ago

TLE from 2 weeks ago
0 FALCON 9 R/B
1 61184U 24167C   26155.21769683  .00000041  00000-0  00000-0 0  9996
2 61184  55.1968 221.2229 0010432  15.6881 344.4356  1.72615540 10758
Epoch: 2026-06-04T05:13Z
TLE epoch observation values (Epoch: 2026-06-04T05:13:29.006Z)
Latitude
0.00004°
Longitude
-109.80316°
Altitude
22,947.599 km
Speed
3.689 km/s
True Right ascension
14h 44m 55s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
07:18:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
23,007.476 km
Perigee altitude
22,946.229 km
Semi-major axis
29,354.989 km
Eccentricity
0.00104
Inclination
55.1968°
RAAN
221.2229°
Arg. of periapsis
15.6881°
True anomaly
344.40348°
Mean anomaly
344.4356°
Eccentric anomaly
344.41955°
Mean motion
0.43154 °/min
Orbital period
834.22 mins
BSTAR
0
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Other satellites on launch #167 in the year 2024 (2024-09-17 UTC)

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