DELTA 1 R/B, 738

Orbit data source: Space-Track

DELTA 1 R/B, 738 is space debris originally from a launch on Tue, 21 Jan 1964 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
738, 1964-003B
Orbit
Active
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)
1964-01-21 (62 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: 2 days ago

TLE from 2 days ago
0 DELTA 1 R/B
1 00738U 64003B   25309.51403993 -.00000023  00000-0  00000-0 0  9990
2 00738  46.4502 245.6696 2601792 122.9885 264.7967  7.39344153668933
Epoch: 2025-11-05T12:20Z
TLE epoch observation values (Epoch: 2025-11-05T12:20:13.049Z)
Latitude
-0.00004°
Longitude
15.62957°
Altitude
5,708.327 km
Speed
5.492 km/s
True Right ascension
16h 22m 40s
True Declination
0° 00' 00"
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
03:17:53
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
7,649.129 km
Perigee altitude
1,856.932 km
Semi-major axis
11,131.167 km
Eccentricity
0.26018
Inclination
46.4502°
RAAN
245.6696°
Arg. of periapsis
122.9885°
True anomaly
237.07144°
Mean anomaly
264.7967°
Eccentric anomaly
250.72514°
Mean motion
1.84813 °/min
Orbital period
194.79 mins
BSTAR
0
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Other satellites on launch #3 in the year 1964 (1964-01-21 UTC)

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