IUS DEB, 26076

Orbit data source: Space-Track

IUS DEB, 26076 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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Iframe URL

https://www.satcat.com/sats-embedded/26076?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26076, 1999-040E

Orbit

Active

Country

Related business

National Aeronautics and Space Administration (NASA) (US)

Manufacturer

Boeing/Kent

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1999-07-23 (27 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.1 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago

0 IUS DEB
1 26076U 99040E   26170.35380264  .00001159  00000-0  37501-3 0  9995
2 26076  28.3954 189.7701 4312471   0.6266 359.7888  6.70515917528227

Epoch: 2026-06-19T08:29Z

TLE epoch observation values (Epoch: 2026-06-19T08:29:28.548Z)

Latitude

-0°

Longitude

154.81716°

Altitude

377.73 km

Speed

9.19 km/s

True Right ascension

12h 39m 04s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

Unknown

Longitude

Unknown

Altitude

Unknown

Speed

Unknown

Apparent Right ascension

Unknown

Apparent Declination

Unknown

Sunlit

N/A

Visualization observer readout

Local Sidereal Time

00:50:41

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,629.055 km

Perigee altitude

380.228 km

Semi-major axis

11,882.778 km

Eccentricity

0.43125

Inclination

28.3954°

RAAN

189.7701°

Arg. of periapsis

0.6266°

True anomaly

359.41094°

Mean anomaly

359.7888°

Eccentric anomaly

359.62866°

Mean motion

1.67558 °/min

Orbital period

214.85 mins

BSTAR

0.00037501

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Other satellites on launch #40 in the year 1999 (1999-07-23 UTC)

STS 93, 25866 (Decayed)

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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.
8 mins	2026-06-22 13:48:07.914Z	162.546° S	2026-06-22 13:48:07.914Z	162.546° S	14.696°	2026-06-22 13:56:07.914Z	158.889° S
26 mins	2026-06-23 05:45:07.914Z	214.082° SW	2026-06-23 05:50:07.914Z	154.209° SSE	33.76°	2026-06-23 06:11:07.914Z	94.522° ESE
83 mins	2026-06-23 09:29:07.914Z	258.719° W	2026-06-23 09:45:07.914Z	187.877° SSW	39.359°	2026-06-23 10:52:07.914Z	128.932° SE
25 mins	2026-06-23 13:23:07.914Z	263.598° W	2026-06-23 13:48:07.914Z	230.998° WSW	25.393°	2026-06-23 13:48:07.914Z	230.998° WSW

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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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Check out IUS DEB, 26076 on other resources

View IUS DEB, 26076 on Heavens-Above

View IUS DEB, 26076 on Keep Track

View IUS DEB, 26076 on Celestrak

View IUS DEB, 26076 on Gunter's Space Page

Satcat and Kayhan Space are not affiliated with NASA, Celestrak, Heavens-Above, Keep Track, or Gunter's Space Page.

IUS DEB, 26076

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 3 days ago

TLE from 3 days ago

TLE epoch observation values (Epoch: 2026-06-19T08:29:28.548Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #40 in the year 1999 (1999-07-23 UTC)

IUS DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out IUS DEB, 26076 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 3 days ago