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: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B
1 00341U 62029B   25240.44329309 -.00000164  00000-0 -90789-3 0  9993
2 00341  44.7921  41.9930 2422238  37.0491 352.9530  9.14310450108351
Epoch: 2025-08-28T10:38Z
TLE epoch observation values (Epoch: 2025-08-28T10:38:20.522Z)
Latitude
17.49049°
Longitude
-76.09603°
Altitude
972.502 km
Speed
8.2 km/s
True Right ascension
04h 01m 34s
True Declination
17° 23' 42"
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
15:18:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,624.136 km
Perigee altitude
943.439 km
Semi-major axis
9,661.925 km
Eccentricity
0.24222
Inclination
44.7921°
RAAN
41.993°
Arg. of periapsis
37.0491°
True anomaly
348.12646°
Mean anomaly
352.953°
Eccentric anomaly
350.7134°
Mean motion
2.28532 °/min
Orbital period
157.53 mins
BSTAR
-0.00090789
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Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)

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