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
Last TLE update
11 hours ago
Origin
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

TLE from 11 hours ago
0 DELTA 1 R/B
1 00575U 63013B   25200.95154219 -.00000045  00000-0 -49122-3 0  9997
2 00575  42.7668 277.2303 4013230 169.7331 359.8444  6.40267839454701
Epoch: 2025-07-19T22:50Z
TLE epoch observation values (Epoch: 2025-07-19T22:50:13.245Z)
Latitude
7.22388°
Longitude
168.86092°
Altitude
955.381 km
Speed
8.729 km/s
True Right ascension
05h 57m 35s
True Declination
7° 10' 56"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
22.24563°
Longitude
150.10811°
Altitude
1,143.027 km
Speed
8.574 km/s
Apparent Right ascension
07h 06m 16s
Apparent Declination
-8° 26' 41"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
22:52:20
Azimuth
73.939° E
Elevation
-30.848°
Doppler factor
1
Orbital elements
Apogee altitude
10,791.076 km
Perigee altitude
956.941 km
Semi-major axis
12,252.145 km
Eccentricity
0.40132
Inclination
42.7668°
RAAN
277.2303°
Arg. of periapsis
169.7331°
True anomaly
359.60236°
Mean anomaly
359.8444°
Eccentric anomaly
359.74009°
Mean motion
1.60039 °/min
Orbital period
224.95 mins
BSTAR
-0.00049122
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