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   25258.25192429 -.00000076  00000-0 -11318-2 0  9997
2 00575  42.7581 216.4948 4016120 239.7724 315.4892  6.40269232458371
Epoch: 2025-09-15T06:02Z
TLE epoch observation values (Epoch: 2025-09-15T06:02:46.258Z)
Latitude
19.4189°
Longitude
-70.97701°
Altitude
3,827.328 km
Speed
6.753 km/s
True Right ascension
00h 56m 41s
True Declination
19° 20' 37"
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
07:00:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,794.594 km
Perigee altitude
953.39 km
Semi-major axis
12,252.129 km
Eccentricity
0.40161
Inclination
42.7581°
RAAN
216.4948°
Arg. of periapsis
239.7724°
True anomaly
270.96576°
Mean anomaly
315.4892°
Eccentric anomaly
294.56046°
Mean motion
1.60039 °/min
Orbital period
224.95 mins
BSTAR
-0.0011318
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Other satellites on launch #13 in the year 1963 (1963-05-07 UTC)

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