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 (64 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 23 hours ago

TLE from 23 hours ago
0 DELTA 1 R/B
1 00341U 62029B   26149.74083304  .00000083  00000-0  79636-3 0  9993
2 00341  44.7980 249.8590 2424697 224.2119 321.0183  9.14327517133446
Epoch: 2026-05-29T17:46Z
TLE epoch observation values (Epoch: 2026-05-29T17:46:47.974Z)
Latitude
11.87824°
Longitude
-96.27687°
Altitude
1,762.349 km
Speed
7.53 km/s
True Right ascension
03h 50m 45s
True Declination
11° 49' 04"
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
01:55:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,626.361 km
Perigee altitude
940.972 km
Semi-major axis
9,661.804 km
Eccentricity
0.24247
Inclination
44.798°
RAAN
249.859°
Arg. of periapsis
224.2119°
True anomaly
298.82205°
Mean anomaly
321.0183°
Eccentric anomaly
310.44584°
Mean motion
2.28537 °/min
Orbital period
157.52 mins
BSTAR
0.00079636
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Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)

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