DELTA 2 R/B, 40060

Orbit data source: Space-Track

DELTA 2 R/B, 40060 is space debris in HEO originally from a launch on Wed, 02 Jul 2014 UTC launched from the Air Force Western Test Range (AFWTR). 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
40060, 2014-035B
Orbit
HEO
Country
Flag of USUS
Related business
Manufacturer
Boeing/Pueblo
Mission
Spacecraft
Bus & Motor
DELTA/0020, Unknown motor
Mass
~924 kg wet, 924 kg dry
Launch date (UTC)
2014-07-02 (11 years ago)
Launch vehicle
Unknown
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl + Cone, 3.0 m
Radar Cross Section
13.836 m², Large (>1 m²)

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

TLE from 2 days ago
0 DELTA 2 R/B
1 40060U 14035B   25337.20743426 -.00000012  00000-0  00000+0 0  9994
2 40060  98.2175  64.4648 3078466 233.9377  93.5811  6.11240449254924
Epoch: 2025-12-03T04:58Z
TLE epoch observation values (Epoch: 2025-12-03T04:58:42.320Z)
Latitude
-0.00006°
Longitude
-82.48554°
Altitude
7,598.254 km
Speed
5.05 km/s
True Right ascension
04h 17m 53s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
05:57:57
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,144.736 km
Perigee altitude
2,366.285 km
Semi-major axis
12,633.648 km
Eccentricity
0.30785
Inclination
98.2175°
RAAN
64.4648°
Arg. of periapsis
233.9377°
True anomaly
126.13359°
Mean anomaly
93.5811°
Eccentric anomaly
110.14081°
Mean motion
1.52845 °/min
Orbital period
235.53 mins
BSTAR
0
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Other satellites on launch #35 in the year 2014 (2014-07-02 UTC)

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