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.
Focus sentinelFocus sentinel
2971 intel report (Beta)
DELTA 1 R/B(2) * details
Identifier | |
Orbit | HEO |
Last TLE update | 16 hours ago |
Origin | |
Manufacturer | UTC |
Mission | Spacecraft |
Bus & Motor | FW4, Unknown motor |
Mass | ~40 kg wet, ~40 kg dry |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Cyl, 1.5 m |
Radar Cross Section | 0.687 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 16 hours ago
0 DELTA 1 R/B(2) *
1 2971U 67094C 25044.00217253 .00003227 00000-0 22683-2 0 9997
2 2971 28.2997 87.1995 6560784 38.6850 353.6683 3.18458686544201
Epoch: 2025-02-13T00:03Z
Definitive object data (Epoch: 2025-02-13T00:03:07.706Z)
Latitude | -0.00007° |
Longitude | -56.81388° |
Altitude | 958.254 km |
Speed | 9.393 km/s |
True Right ascension | 05h 49m 00s |
True Declination | 0° 00' 00" |
Sunlit | Object was in partial shadow at TLE epoch |
Visualization TLE readout
Latitude | 25.15456° |
Longitude | 62.63603° |
Altitude | 3,338.7 km |
Speed | 7.851 km/s |
Apparent Right ascension | 11h 33m 30s |
Apparent Declination | 0° 18' 06" |
Sunlit | Object is in daylight |
Visualization observer readout
Local Sidereal Time | 18:10:43 |
Azimuth | 276.234° WNW |
Elevation | -6.929° |
Doppler factor | 1 |
Orbital elements
Apogee altitude | 25,945.86 km |
Perigee altitude | 334.662 km |
Semi-major axis | 19,518.398 km |
Eccentricity | 0.6560784 |
Inclination | 28.2997° |
RAAN | 87.1995° |
Arg. of periapsis | 38.685° |
True anomaly | 321.94864° |
Mean anomaly | 353.6683° |
Eccentric anomaly | 342.13888° |
Mean motion | 0.79593 °/min |
BSTAR | 0.0022683 |
Orbital period | 452.3 mins |
Loading maneuver chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Other satellites on launch #94 in the year 1967 (1967-09-28 UTC)
INTELSAT 2-F4, 2969 |
DELTA 1 R/B(1), 2970 (Decayed) |
DELTA 1 R/B(2) *, 2971 |
DELTA 1 DEB, 2972 (Decayed) |
DELTA 1 R/B(2) * Visibility forecast
Observer location: undefined°, undefined
Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
---|---|---|---|---|---|---|---|
281 mins | 2025-02-13 15:44:30.321Z | 259.657° W | 2025-02-13 16:28:30.321Z | 216.49° SW | 27.725° | 2025-02-13 20:25:30.321Z | 202.505° SW |
81 mins | 2025-02-14 14:14:30.321Z | 256.334° W | 2025-02-14 14:42:30.321Z | 201.446° SSW | 33.097° | 2025-02-14 15:35:30.321Z | 179.745° S |
Authenticating...
Click to sort rows by NORAD ID header in ascending order | Click to sort rows by Common name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|