DELTA 2 R/B, 40060
Orbit data source: Space-Track
DELTA 2 R/B, 40060 is space debris in HEO originally from a launch on Wed, 02 Jul 2014 UTC launched from the Air Force Western Test Range (AFWTR). 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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40060 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/Pueblo
Mission
Spacecraft
Bus & Motor
DELTA/0020, Unknown motor
Mass
~924 kg wet, 924 kg dry
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Cyl + Cone, 3.0 m
Radar Cross Section
13.836 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 DELTA 2 R/B
1 40060U 14035B 25258.33265513 .00000030 00000-0 00000-0 0 9996
2 40060 98.2145 51.9475 3068032 273.2819 52.6845 6.11238283250108Epoch: 2025-09-15T07:59Z
TLE epoch observation values (Epoch: 2025-09-15T07:59:01.403Z)
Latitude
-0.00007°
Longitude
-62.3502°
Altitude
4,877.037 km
Speed
6.269 km/s
True Right ascension
03h 27m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
13:58:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,131.596 km
Perigee altitude
2,379.489 km
Semi-major axis
12,633.68 km
Eccentricity
0.3068
Inclination
98.2145°
RAAN
51.9475°
Arg. of periapsis
273.2819°
True anomaly
86.79337°
Mean anomaly
52.6845°
Eccentric anomaly
69.10723°
Mean motion
1.52844 °/min
Orbital period
235.53 mins
BSTAR
0
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Other satellites on launch #35 in the year 2014 (2014-07-02 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.DELTA 2 R/B Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 73 mins | 2025-09-15 21:18:29.311Z | 16.918° NNE | 2025-09-15 22:01:29.311Z | 94.406° ESE | 42.146° | 2025-09-15 22:31:29.311Z | 175.03° S |
| 85 mins | 2025-09-16 00:49:29.311Z | 14.732° NNE | 2025-09-16 01:38:29.311Z | 319.695° NNW | 36.918° | 2025-09-16 02:14:29.311Z | 255.06° W |
| 71 mins | 2025-09-16 04:21:29.311Z | 41.674° NE | 2025-09-16 04:55:29.311Z | 1.393° NNE | 25.31° | 2025-09-16 05:32:29.311Z | 320.124° NNW |
| 83 mins | 2025-09-16 07:41:29.311Z | 110.548° ESE | 2025-09-16 08:13:29.311Z | 44.145° NE | 38.293° | 2025-09-16 09:04:29.311Z | 345.96° N |
| 84 mins | 2025-09-16 11:27:29.311Z | 194.928° SSW | 2025-09-16 11:54:29.311Z | 270.875° WNW | 40.093° | 2025-09-16 12:51:29.311Z | 353.347° N |
| 41 mins | 2025-09-16 20:37:29.311Z | 7.192° NNE | 2025-09-16 21:18:29.311Z | 45.079° ENE | 36.191° | 2025-09-16 21:18:29.311Z | 45.079° ENE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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