DELTA 1 R/B, 1433

Orbit data source: Space-Track

DELTA 1 R/B, 1433 is space debris in SSO originally from a launch on Fri, 02 Jul 1965 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
1433, 1965-051B
Orbit
SSO
Country
Flag of USUS
Related business
Manufacturer
ABL
Mission
Spacecraft
Bus & Motor
ALTAIR, Unknown motor
Mass
60 kg wet, 60 kg dry
Launch date (UTC)
1965-07-02 (60 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
0.687 m², Medium (>0.1 m² and < 1m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 DELTA 1 R/B
1 01433U 65051B   25242.89598193  .00001878  00000-0  38197-3 0  9990
2 01433  98.5371  27.0017 0040403  93.9565 266.6256 14.61828359152403
Epoch: 2025-08-30T21:30Z
TLE epoch observation values (Epoch: 2025-08-30T21:30:12.838Z)
Latitude
0.00003°
Longitude
85.1245°
Altitude
692.049 km
Speed
7.509 km/s
True Right ascension
01h 48m 00s
True Declination
0° 00' 00"
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
19:24:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
712.906 km
Perigee altitude
655.836 km
Semi-major axis
7,062.508 km
Eccentricity
0.00404
Inclination
98.5371°
RAAN
27.0017°
Arg. of periapsis
93.9565°
True anomaly
266.16356°
Mean anomaly
266.6256°
Eccentric anomaly
266.39457°
Mean motion
3.65683 °/min
Orbital period
98.45 mins
BSTAR
0.00038197
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Other satellites on launch #51 in the year 1965 (1965-07-02 UTC)

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