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   25348.17202701 -.00000030  00000-0  00000-0 0  9999
2 40060  98.2167  66.2079 3079756 228.4816 100.7819  6.11240605255590
Epoch: 2025-12-14T04:07Z
TLE epoch observation values (Epoch: 2025-12-14T04:07:43.133Z)
Latitude
-0.00002°
Longitude
-78.80493°
Altitude
7,998.854 km
Speed
4.89 km/s
True Right ascension
04h 24m 51s
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
12:40:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,146.363 km
Perigee altitude
2,364.654 km
Semi-major axis
12,633.645 km
Eccentricity
0.30798
Inclination
98.2167°
RAAN
66.2079°
Arg. of periapsis
228.4816°
True anomaly
131.58761°
Mean anomaly
100.7819°
Eccentric anomaly
116.56474°
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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