DELTA 1 R/B(2) *, 2971

Orbit data source: Space-Track

DELTA 1 R/B(2) *, 2971 is space debris in HEO originally from a launch on Thu, 28 Sep 1967 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
2971, 1967-094C
Orbit
HEO
Last TLE update
1 day ago
Origin
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
1967-09-28 (58 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, Large (>1 m²)

Expand to show TLE details & history

TLE from 1 day ago
0 DELTA 1 R/B(2) *
1 02971U 67094C   25198.72940833  .00004788  00000-0  28433-2 0  9995
2 02971  28.4063   3.3291 6557206 175.3861 196.8377  3.19426746549072
Epoch: 2025-07-17T17:30Z
TLE epoch observation values (Epoch: 2025-07-17T17:30:20.879Z)
Latitude
-0.00003°
Longitude
164.95037°
Altitude
25,653.91 km
Speed
2.103 km/s
True Right ascension
00h 13m 18s
True Declination
0° 00' 00"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
-2.29908°
Longitude
160.02727°
Altitude
25,841.009 km
Speed
2.068 km/s
Apparent Right ascension
23h 53m 42s
Apparent Declination
-8° 13' 30"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
11:54:16
Azimuth
0.269° NNE
Elevation
-58.309°
Doppler factor
1
Orbital elements
Apogee altitude
25,873.545 km
Perigee altitude
328.061 km
Semi-major axis
19,478.94 km
Eccentricity
0.65572
Inclination
28.4063°
RAAN
3.3291°
Arg. of periapsis
175.3861°
True anomaly
184.65663°
Mean anomaly
196.8377°
Eccentric anomaly
190.19065°
Mean motion
0.79835 °/min
Orbital period
450.93 mins
BSTAR
0.0028433
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