FALCON 9 R/B, 58699

Orbit data source: Space-Track

FALCON 9 R/B, 58699 is space debris in HEO originally from a launch on Wed, 03 Jan 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
58699, 2024-003B
Orbit
HEO
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)
2024-01-03 (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: 6 days ago

TLE from 6 days ago
0 FALCON 9 R/B
1 58699U 24003B   26167.46639815  .00001341  00000-0  18475-2 0  9996
2 58699  27.0096  55.8244 7706782 218.5456  47.3823  1.74494796 15193
Epoch: 2026-06-16T11:11Z
TLE epoch observation values (Epoch: 2026-06-16T11:11:36.800Z)
Latitude
-0.00001°
Longitude
-16.72511°
Altitude
23,415.285 km
Speed
3.617 km/s
True Right ascension
03h 43m 39s
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
21:36:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
45,233.409 km
Perigee altitude
306.111 km
Semi-major axis
29,147.897 km
Eccentricity
0.77068
Inclination
27.0096°
RAAN
55.8244°
Arg. of periapsis
218.5456°
True anomaly
141.37571°
Mean anomaly
47.3823°
Eccentric anomaly
91.5233°
Mean motion
0.43615 °/min
Orbital period
825.41 mins
BSTAR
0.0018475
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Other satellites on launch #3 in the year 2024 (2024-01-03 UTC)

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