DELTA 1 R/B, 341

Orbit data source: Space-Track

DELTA 1 R/B, 341 is space debris in LEO originally from a launch on Tue, 10 Jul 1962 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
341, 1962-029B
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
24 kg wet, 24 kg dry
Launch date (UTC)
1962-07-10 (63 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 0.8 m
Radar Cross Section
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B
1 00341U 62029B   25257.39381693 -.00000203  00000-0 -11801-2 0  9990
2 00341  44.7974  10.3452 2421912  70.8598 345.8072  9.14306442109909
Epoch: 2025-09-14T09:27Z
TLE epoch observation values (Epoch: 2025-09-14T09:27:05.782Z)
Latitude
31.21265°
Longitude
-87.67191°
Altitude
1,066.347 km
Speed
8.119 km/s
True Right ascension
03h 10m 51s
True Declination
31° 04' 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
12:22:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,623.855 km
Perigee altitude
943.775 km
Semi-major axis
9,661.952 km
Eccentricity
0.24219
Inclination
44.7974°
RAAN
10.3452°
Arg. of periapsis
70.8598°
True anomaly
336.28712°
Mean anomaly
345.8072°
Eccentric anomaly
341.37554°
Mean motion
2.28531 °/min
Orbital period
157.53 mins
BSTAR
-0.0011801
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Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)

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