DELTA 1 R/B, 4903

Orbit data source: Space-Track

DELTA 1 R/B, 4903 is space debris in HEO originally from a launch on Wed, 03 Feb 1971 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
4903, 1971-009B
Orbit
HEO
Last TLE update
22 hours ago
Origin
Manufacturer
Thiokol/TE
Mission
Spacecraft
Bus & Motor
STAR 37, Unknown motor
Mass
65 kg wet, 65 kg dry
Launch date (UTC)
1971-02-03 (54 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Sphere + Cone, 0.5 m
Radar Cross Section
0.734 m², Large (>1 m²)

Expand to show TLE details & history

TLE from 22 hours ago
0 DELTA 1 R/B
1  4903U 71009B   25196.76788655  .00002526  00000-0  89944-3 0  9990
2  4903  25.6427  51.1861 5844613 208.8898  99.7727  4.23929843583045
Epoch: 2025-07-15T18:25Z
TLE epoch observation values (Epoch: 2025-07-15T18:25:45.397Z)
Latitude
-0.00005°
Longitude
-159.09513°
Altitude
15,363.025 km
Speed
3.457 km/s
True Right ascension
03h 24m 48s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-3.56779°
Longitude
-167.29361°
Altitude
13,206.056 km
Speed
3.999 km/s
Apparent Right ascension
02h 08m 18s
Apparent Declination
-18° 17' 55"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
05:24:52
Azimuth
228.32° WSW
Elevation
15.957°
Doppler factor
1
Orbital elements
Apogee altitude
19,179.464 km
Perigee altitude
324.565 km
Semi-major axis
16,130.151 km
Eccentricity
0.58446
Inclination
25.6427°
RAAN
51.1861°
Arg. of periapsis
208.8898°
True anomaly
Unknown
Mean anomaly
99.7727°
Eccentric anomaly
Unknown
Mean motion
1.05946 °/min
Orbital period
339.8 mins
BSTAR
0.00089944
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