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 (26 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

Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 months ago

TLE from 2 months ago

0 IUS DEB
1 26076U 99040E   25285.95899685  .00002424  00000-0  68643-3 0  9996
2 26076  28.4019 204.6564 4329631 109.7817 301.0621  6.69521389511497

Epoch: 2025-10-12T23:00Z

TLE epoch observation values (Epoch: 2025-10-12T23:00:57.327Z)

Latitude

-0.00004°

Longitude

-162.35119°

Altitude

4,937.343 km

Speed

6.078 km/s

True Right ascension

13h 38m 37s

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

22:56:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

10,666.307 km

Perigee altitude

366.509 km

Semi-major axis

11,894.545 km

Eccentricity

0.43296

Inclination

28.4019°

RAAN

204.6564°

Arg. of periapsis

109.7817°

True anomaly

250.26699°

Mean anomaly

301.0621°

Eccentric anomaly

276.41024°

Mean motion

1.6731 °/min

Orbital period

215.17 mins

BSTAR

0.00068643

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

STS 93, 25866 (Decayed)

IUS DEB, 29037

IUS DEB, 43363

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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.
19 mins	2025-12-27 06:10:51.026Z	132.038° SE	2025-12-27 06:17:51.026Z	112.165° ESE	12.636°	2025-12-27 06:29:51.026Z	91.987° ESE
106 mins	2025-12-27 09:46:51.026Z	223.502° SW	2025-12-27 10:10:51.026Z	150.352° SSE	40.85°	2025-12-27 11:32:51.026Z	90.108° ESE
129 mins	2025-12-27 13:38:51.026Z	265.638° W	2025-12-27 14:39:51.026Z	199.751° SSW	42.665°	2025-12-27 15:47:51.026Z	128.3° SE
94 mins	2025-12-27 17:58:51.026Z	280.392° WNW	2025-12-27 18:59:51.026Z	239.699° WSW	26.058°	2025-12-27 19:32:51.026Z	188.771° SSW

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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: 2 months ago

TLE from 2 months ago

TLE epoch observation values (Epoch: 2025-10-12T23:00:57.327Z)

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: 2 months ago