IUS DEB, 43365

Orbit data source: Space-Track

IUS DEB, 43365 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/43365?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43365, 1999-040N

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: 1 month ago

TLE from 1 month ago

0 IUS DEB
1 43365U 99040N   26227.13652096  .00000017  00000-0  00000-0 0  9992
2 43365  27.6632 161.1440 2805587 175.4762 187.7810  7.21616467357235

Epoch: 2026-08-15T03:16Z

TLE epoch observation values (Epoch: 2026-08-15T03:16:35.410Z)

Latitude

-0.00003°

Longitude

148.44468°

Altitude

8,087.778 km

Speed

4.459 km/s

True Right ascension

10h 44m 34s

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

15:59:59

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

8,111.084 km

Perigee altitude

1,762.172 km

Semi-major axis

11,314.765 km

Eccentricity

0.28056

Inclination

27.6632°

RAAN

161.144°

Arg. of periapsis

175.4762°

True anomaly

184.55817°

Mean anomaly

187.781°

Eccentric anomaly

186.07875°

Mean motion

1.80333 °/min

Orbital period

199.63 mins

BSTAR

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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.
38 mins	2026-09-22 22:53:13.412Z	228.343° WSW	2026-09-22 23:00:13.412Z	208.366° SW	56.084°	2026-09-22 23:31:13.412Z	137.166° SSE
33 mins	2026-09-23 02:22:13.412Z	267.422° W	2026-09-23 02:42:13.412Z	236.278° WSW	17.173°	2026-09-23 02:55:13.412Z	203.803° SW
63 mins	2026-09-23 13:57:13.412Z	185.399° SSW	2026-09-23 14:20:13.412Z	130.231° SE	31.609°	2026-09-23 15:00:13.412Z	82.255° E
93 mins	2026-09-23 17:29:13.412Z	236.558° WSW	2026-09-23 18:09:13.412Z	162.566° S	64.632°	2026-09-23 19:02:13.412Z	94.476° ESE
90 mins	2026-09-23 21:15:13.412Z	268.859° W	2026-09-23 22:09:13.412Z	202.156° SSW	61.236°	2026-09-23 22:45:13.412Z	128.44° SE

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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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Check out IUS DEB, 43365 on other resources

View IUS DEB, 43365 on Heavens-Above

View IUS DEB, 43365 on Keep Track

View IUS DEB, 43365 on Celestrak

View IUS DEB, 43365 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, 43365

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 1 month ago

TLE from 1 month ago

TLE epoch observation values (Epoch: 2026-08-15T03:16:35.410Z)

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, 43365 on other resources

Documentation

Expand to show TLE details & history
Last TLE update: 1 month ago