IUS DEB, 26078
Orbit data source: Space-Track
IUS DEB, 26078 is space debris originally from a launch on Fri, 23 Jul 1999 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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26078 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
Boeing/Kent
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 7 months ago
TLE from 7 months ago
0 IUS DEB
1 26078U 99040F 25056.87963623 .00008656 00000-0 20332-2 0 9994
2 26078 28.3946 251.8912 4386130 170.9622 200.7601 6.61930195461723Epoch: 2025-02-25T21:06Z
TLE epoch observation values (Epoch: 2025-02-25T21:06:40.57Z)
Latitude
0.00003°
Longitude
139.24502°
Altitude
10,690.445 km
Speed
3.667 km/s
True Right ascension
16h 47m 33s
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
16:51:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
10,864.06 km
Perigee altitude
350.25 km
Semi-major axis
11,985.292 km
Eccentricity
0.43861
Inclination
28.3946°
RAAN
251.8912°
Arg. of periapsis
170.9622°
True anomaly
189.07323°
Mean anomaly
200.7601°
Eccentric anomaly
194.47746°
Mean motion
1.65413 °/min
Orbital period
217.64 mins
BSTAR
0.0020332
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Other satellites on launch #40 in the year 1999 (1999-07-23 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.IUS DEB 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. |
|---|---|---|---|---|---|---|---|
| 58 mins | 2025-09-14 04:59:33.042Z | 175.455° S | 2025-09-14 05:13:33.042Z | 124.274° SE | 26.058° | 2025-09-14 05:57:33.042Z | 78.919° E |
| 122 mins | 2025-09-14 08:44:33.042Z | 241.878° WSW | 2025-09-14 09:18:33.042Z | 166.237° S | 42.994° | 2025-09-14 10:46:33.042Z | 101.633° ESE |
| 126 mins | 2025-09-14 12:44:33.042Z | 273.997° WNW | 2025-09-14 13:56:33.042Z | 216.124° SW | 40.015° | 2025-09-14 14:50:33.042Z | 146.293° SSE |
| 42 mins | 2025-09-14 17:39:33.042Z | 270.089° WNW | 2025-09-14 18:04:33.042Z | 251.191° W | 12.772° | 2025-09-14 18:21:33.042Z | 230.666° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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