FALCON 9 R/B, 41590

Orbit data source: Space-Track

FALCON 9 R/B, 41590 is space debris in HEO originally from a launch on Wed, 15 Jun 2016 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
41590, 2016-038C
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)
2016-06-15 (10 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: 1 day ago

TLE from 1 day ago
0 FALCON 9 R/B
1 41590U 16038C   25354.43559801  .00001158  00000-0  21180-2 0  9990
2 41590  23.7674   0.0978 7967870 242.1610  19.5910  1.45625652 43462
Epoch: 2025-12-20T10:27Z
TLE epoch observation values (Epoch: 2025-12-20T10:27:15.668Z)
Latitude
-0.00015°
Longitude
114.02435°
Altitude
12,630.922 km
Speed
5.46 km/s
True Right ascension
00h 00m 24s
True Declination
0° 00' 01"
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
13:56:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
52,705.53 km
Perigee altitude
304.107 km
Semi-major axis
32,882.956 km
Eccentricity
0.79679
Inclination
23.7674°
RAAN
0.0978°
Arg. of periapsis
242.161°
True anomaly
118.05841°
Mean anomaly
19.591°
Eccentric anomaly
58.52772°
Mean motion
0.36399 °/min
Orbital period
989.04 mins
BSTAR
0.002118
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Other satellites on launch #38 in the year 2016 (2016-06-15 UTC)

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