DELTA 1 R/B, 1729
Orbit data source: Space-Track
DELTA 1 R/B, 1729 is space debris in LEO originally from a launch on Sat, 06 Nov 1965 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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1729 intel report
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DELTA 1 R/B details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 22 hours ago |
| Origin | |
| Manufacturer | ABL |
| Mission | Spacecraft |
| Bus & Motor | ALTAIR, Unknown motor |
| Mass | ~60 kg wet, ~60 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 22 hours ago
0 DELTA 1 R/B
1 01729U 65089B 24285.81719221 -.00000065 00000-0 65138-4 0 9998
2 01729 59.3912 312.7667 0716042 149.7255 20.1134 11.97555551576952Epoch: 2024-10-11T19:36Z
Definitive object data (Epoch: 2024-10-11T19:36:45.406Z)
| Latitude | 6.04613° |
| Longitude | 174.1215° |
| Altitude | 1,155.353 km |
| Speed | 7.514 km/s |
| True Right ascension | 08h 36m 46s |
| True Declination | 6° 00' 44" |
| Sunlit | Object was in daylight at TLE epoch |
Predictive object data (real-time)
| Latitude | -28.64306° |
| Longitude | -165.63403° |
| Altitude | 1,409.142 km |
| Speed | 7.284 km/s |
| Apparent Right ascension | 06h 58m 18s |
| Apparent Declination | -62° 50' 26" |
| Sunlit | Object is in daylight |
Predictive observer data (real-time)
| Local Sidereal Time | 12:18:11 |
| Azimuth | 211.503° SW |
| Elevation | -30.66° |
| Doppler factor | 1 |
Orbital elements
| Apogee | 2,269.017 km |
| Perigee | 1,113.418 km |
| Semi-major axis | 8,069.354 km |
| Eccentricity | 0.0716042 |
| Inclination | 59.3912° |
| RAAN | 312.7667° |
| Arg. of periapsis | 149.7255° |
| True anomaly | 23.19136° |
| Mean anomaly | 20.1134° |
| Eccentric anomaly | 21.62536° |
| Mean motion | 2.99423 °/min |
| BSTAR | 0.000065138 |
| Period | 120.23 mins |
No data available
No data available
Other satellites on launch #89 in the year 1965 (1965-11-06 UTC)
| EXPLORER 29 (GEOS 1), 1726 |
| DELTA 1 R/B, 1729 |
| DELTA 1 DEB, 2700 |
| DELTA 1 DEB, 2888 |
| DELTA 1 DEB, 27788 |
| DELTA 1 DEB, 27789 |
| DELTA 1 DEB, 28662 |
| DELTA 1 DEB, 29010 |
DELTA 1 R/B Visibility forecast
Observer location: 39.9160978°, -105.1181434
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. |
|---|---|---|---|---|---|---|---|
| 19 mins | 2024-10-13 02:49:28.832Z | 187.024° SSW | 2024-10-13 02:59:28.832Z | 124.576° SE | 36.567° | 2024-10-13 03:08:28.832Z | 51.468° ENE |
| 18 mins | 2024-10-13 04:55:28.832Z | 241.677° WSW | 2024-10-13 05:05:28.832Z | 323.731° NNW | 39.912° | 2024-10-13 05:13:28.832Z | 34.106° NE |
| 12 mins | 2024-10-13 07:06:28.832Z | 298.334° NW | 2024-10-13 07:12:28.832Z | 342.544° N | 21.903° | 2024-10-13 07:18:28.832Z | 31.691° NE |
| 9 mins | 2024-10-13 09:16:28.832Z | 335° NNW | 2024-10-13 09:20:28.832Z | 8.845° NNE | 20.28° | 2024-10-13 09:25:28.832Z | 56.545° ENE |
| 13 mins | 2024-10-13 11:21:28.832Z | 326.825° NNW | 2024-10-13 11:27:28.832Z | 29.025° NE | 39.847° | 2024-10-13 11:34:28.832Z | 121.547° SE |
| 10 mins | 2024-10-13 13:27:28.832Z | 294.215° NW | 2024-10-13 13:32:28.832Z | 240.232° WSW | 25.018° | 2024-10-13 13:37:28.832Z | 190.531° SSW |