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
Country
Flag of USUS
Related business
Manufacturer
UTC
Mission
Spacecraft
Bus & Motor
FW4, Unknown motor
Mass
~40 kg wet, ~40 kg dry
Launch date (UTC)
1967-09-28 (59 years ago)
Launch vehicle
Unknown
Launch site
Air Force Eastern Test Range (AFETR)
Object type
Payload
Rocket body
Debris
Shape & HBR
CYL, 1.1 m
Radar Cross Section
Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 DELTA 1 R/B(2) *
1  2971U 67094C   26310.46942906  .00001452  00000-0  88710-3 0  9996
2  2971  28.2159  99.5329 6523953 246.0511  35.2936  3.23334524564436
Epoch: 2026-11-06T11:15Z
TLE epoch observation values (Epoch: 2026-11-06T11:15:58.670Z)
Latitude
-0.00002°
Longitude
-115.2173°
Altitude
8,707.362 km
Speed
5.676 km/s
True Right ascension
06h 37m 51s
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
10:51:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
25,548.973 km
Perigee altitude
338.182 km
Semi-major axis
19,321.714 km
Eccentricity
0.6524
Inclination
28.2159°
RAAN
99.5329°
Arg. of periapsis
246.0511°
True anomaly
114.07034°
Mean anomaly
35.2936°
Eccentric anomaly
70.53715°
Mean motion
0.80812 °/min
Orbital period
445.48 mins
BSTAR
0.0008871
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Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)

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