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
Unknown
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 15 hours ago

TLE from 15 hours ago
0 DELTA 1 R/B
1   341U 62029B   25289.09400867 -.00000136  00000-0 -71761-3 0  9994
2   341  44.7921 311.1677 2421844 134.0763 286.6870  9.14299352112805
Epoch: 2025-10-16T02:15Z
TLE epoch observation values (Epoch: 2025-10-16T02:15:22.349Z)
Latitude
22.49824°
Longitude
-82.98368°
Altitude
3,167.191 km
Speed
6.504 km/s
True Right ascension
22h 22m 52s
True Declination
22° 24' 27"
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
11:29:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
5,623.852 km
Perigee altitude
943.879 km
Semi-major axis
9,662.003 km
Eccentricity
0.24218
Inclination
44.7921°
RAAN
311.1677°
Arg. of periapsis
134.0763°
True anomaly
258.74459°
Mean anomaly
286.687°
Eccentric anomaly
272.82775°
Mean motion
2.2853 °/min
Orbital period
157.53 mins
BSTAR
-0.00071761
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Other satellites on launch #29 in the year 1962 (1962-07-10 UTC)

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