GLOBALSTAR M004 DEB, 43356

Orbit data source: Space-Track

GLOBALSTAR M004 DEB, 43356 is space debris in LEO originally from a launch on Sat, 14 Feb 1998 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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https://www.satcat.com/sats-embedded/43356?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

43356, 1998-008G

Orbit

LEO

Last TLE update

3 days ago

Origin

Boeing (US)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1998-02-14 (27 years ago)

Launch vehicle

Unknown

Launch site

Air Force Eastern Test Range (AFETR)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown

Radar Cross Section

Small (<0.1 m²)

Expand to show TLE details & history

TLE from 3 days ago

0 GLOBALSTAR M004 DEB
1 43356U 98008G   25196.94360545  .00000355  00000-0  20822-2 0  9994
2 43356  51.9028  70.8880 0033604 199.0627 160.8989 12.78086083442283

Epoch: 2025-07-15T22:38Z

TLE epoch observation values (Epoch: 2025-07-15T22:38:47.51Z)

Latitude

-0.0001°

Longitude

157.1591°

Altitude

1,374.399 km

Speed

7.161 km/s

True Right ascension

04h 43m 33s

True Declination

0° 00' 00"

Sunlit

Object was in daylight at epoch

Visualization orbit readout

Latitude

-4.53425°

Longitude

-28.75639°

Altitude

1,326.186 km

Speed

7.206 km/s

Apparent Right ascension

18h 50m 30s

Apparent Declination

-31° 59' 07"

Sunlit

Object is in full shadow

Visualization observer readout

Local Sidereal Time

11:43:42

Azimuth

107.096° ESE

Elevation

-31.793°

Doppler factor

Orbital elements

Apogee altitude

1,375.553 km

Perigee altitude

1,323.616 km

Semi-major axis

7,727.721 km

Eccentricity

0.00336

Inclination

51.9028°

RAAN

70.888°

Arg. of periapsis

199.0627°

True anomaly

161.02441°

Mean anomaly

160.8989°

Eccentric anomaly

160.96171°

Mean motion

3.19496 °/min

Orbital period

112.68 mins

BSTAR

0.0020822

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Other satellites on launch #8 in the year 1998 (1998-02-14 UTC)

GLOBALSTAR M001, 25162

GLOBALSTAR M004, 25163

GLOBALSTAR M002, 25164

GLOBALSTAR M003, 25165

DELTA 2 R/B, 25166 (Decayed)

GLOBALSTAR DEB, 25350 (Decayed)

GLOBALSTAR M004 DEB, 43357

GLOBALSTAR M004 DEB Visibility forecast

Observer location: undefined°, undefined°

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.
15 mins	2025-07-19 00:22:10.800Z	307.628° NW	2025-07-19 00:30:10.800Z	104.579° ESE	44.839°	2025-07-19 00:37:10.800Z	128.108° SE
11 mins	2025-07-19 02:22:10.800Z	281.759° WNW	2025-07-19 02:27:10.800Z	237.351° WSW	24.357°	2025-07-19 02:33:10.800Z	185.987° SSW
4 mins	2025-07-19 15:01:10.800Z	125.285° SE	2025-07-19 15:02:10.800Z	117.926° SE	12.136°	2025-07-19 15:05:10.800Z	96.513° ESE
15 mins	2025-07-19 16:52:10.800Z	206.539° SW	2025-07-19 16:59:10.800Z	130.615° SE	40.157°	2025-07-19 17:07:10.800Z	57.979° ENE
14 mins	2025-07-19 18:51:10.800Z	261.785° W	2025-07-19 18:57:10.800Z	326.433° NNW	39.274°	2025-07-19 19:05:10.800Z	49.888° ENE
13 mins	2025-07-19 20:51:10.800Z	299.703° NW	2025-07-19 20:57:10.800Z	356.848° N	30.705°	2025-07-19 21:04:10.800Z	61.135° ENE
6 mins	2025-07-19 22:50:10.800Z	311.575° NW	2025-07-19 22:56:10.800Z	1.447° NNE	36.952°	2025-07-19 22:56:10.800Z	1.447° NNE

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 GLOBALSTAR M004 DEB, 43356 on other resources

View GLOBALSTAR M004 DEB, 43356 on Heavens-Above

View GLOBALSTAR M004 DEB, 43356 on Keep Track

View GLOBALSTAR M004 DEB, 43356 on Celestrak

View GLOBALSTAR M004 DEB, 43356 on Gunter's Space Page

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