DELTA 1 R/B, 575

Orbit data source: Space-Track

DELTA 1 R/B, 575 is space debris in HEO originally from a launch on Tue, 07 May 1963 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
575, 1963-013B
Orbit
HEO
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)
1963-05-07 (62 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
0.695 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 00575U 63013B   25260.28142079 -.00000102  00000-0 -15381-2 0  9993
2 00575  42.7589 214.3445 4016183 242.2491 313.4177  6.40268800458506
Epoch: 2025-09-17T06:45Z
TLE epoch observation values (Epoch: 2025-09-17T06:45:14.756Z)
Latitude
19.54792°
Longitude
-85.91677°
Altitude
4,021.486 km
Speed
6.644 km/s
True Right ascension
00h 47m 25s
True Declination
19° 28' 25"
Sunlit
Object was in full shadow 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
00:24:17
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,794.679 km
Perigee altitude
953.316 km
Semi-major axis
12,252.135 km
Eccentricity
0.40162
Inclination
42.7589°
RAAN
214.3445°
Arg. of periapsis
242.2491°
True anomaly
268.28239°
Mean anomaly
313.4177°
Eccentric anomaly
292.09684°
Mean motion
1.60039 °/min
Orbital period
224.95 mins
BSTAR
-0.0015381
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Other satellites on launch #13 in the year 1963 (1963-05-07 UTC)

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