DELTA 1 R/B(2), 2643
Orbit data source: Space-Track
DELTA 1 R/B(2), 2643 is space debris in HEO originally from a launch on Wed, 11 Jan 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
2643 intel report (Beta)
DELTA 1 R/B(2) details
| Identifier | |
| Orbit | HEO |
| Last TLE update | 9 hours ago |
| Origin | |
| Manufacturer | UTC |
| Mission | Spacecraft |
| Bus & Motor | FW4, Unknown motor |
| Mass | 34 kg wet, 34 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, Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 9 hours ago
0 DELTA 1 R/B(2)
1 02643U 67001D 24356.87677167 .00025590 00000-0 59010-2 0 9996
2 02643 25.8055 263.0952 6008372 14.7713 357.0301 4.02118476734037Epoch: 2024-12-21T21:02Z
Definitive object data (Epoch: 2024-12-21T21:02:33.072Z)
| Latitude | 0.00004° |
| Longitude | -143.44985° |
| Altitude | 365.011 km |
| Speed | 9.714 km/s |
| True Right ascension | 17h 32m 26s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -7.61723° |
| Longitude | 52.28539° |
| Altitude | 20,331.003 km |
| Speed | 2.447 km/s |
| Apparent Right ascension | 06h 52m 57s |
| Apparent Declination | -19° 07' 18" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 05:15:06 |
| Azimuth | 154.027° SSE |
| Elevation | 26.707° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 20,368.918 km |
| Perigee altitude | 291.142 km |
| Semi-major axis | 16,708.167 km |
| Eccentricity | 0.6008372 |
| Inclination | 25.8055° |
| RAAN | 263.0952° |
| Arg. of periapsis | 14.7713° |
| True anomaly | 345.22379° |
| Mean anomaly | 357.0301° |
| Eccentric anomaly | 352.59074° |
| Mean motion | 1.00496 °/min |
| BSTAR | 0.005901 |
| Orbital period | 358.22 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 #1 in the year 1967 (1967-01-11 UTC)
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. |
|---|---|---|---|---|---|---|---|
| 77 mins | 2024-12-22 06:10:23.884Z | 154.039° SSE | 2024-12-22 06:10:23.884Z | 154.039° SSE | 24.186° | 2024-12-22 07:27:23.884Z | 151.029° SSE |
| 174 mins | 2024-12-23 03:16:23.884Z | 257.196° W | 2024-12-23 03:39:23.884Z | 190.934° SSW | 38.719° | 2024-12-23 06:10:23.884Z | 152.738° SSE |
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 |
|---|