FALCON 9 R/B, 42968

Orbit data source: Space-Track

FALCON 9 R/B, 42968 is space debris in HEO originally from a launch on Wed, 11 Oct 2017 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
42968, 2017-063B
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)
2017-10-11 (9 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 days ago

TLE from 2 days ago
0 FALCON 9 R/B
1 42968U 17063B   26171.34902642  .00142959  54878-7  13033-2 0  9994
2 42968  27.8474 146.8437 5290943 329.5995   8.1728  5.28999198101660
Epoch: 2026-06-20T08:22Z
TLE epoch observation values (Epoch: 2026-06-20T08:22:35.882Z)
Latitude
-0.00001°
Longitude
112.62369°
Altitude
499.961 km
Speed
9.341 km/s
True Right ascension
09h 47m 21s
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
21:26:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
14,902.036 km
Perigee altitude
175.386 km
Semi-major axis
13,916.848 km
Eccentricity
0.52909
Inclination
27.8474°
RAAN
146.8437°
Arg. of periapsis
329.5995°
True anomaly
30.27036°
Mean anomaly
8.1728°
Eccentric anomaly
17.07288°
Mean motion
1.322 °/min
Orbital period
272.31 mins
BSTAR
0.0013033
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Other satellites on launch #63 in the year 2017 (2017-10-11 UTC)

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