ERS 2 DEB, 35392

Orbit data source: Space-Track

ERS 2 DEB, 35392 is space debris in SSO originally from a launch on Fri, 21 Apr 1995 UTC launched from the French Guiana (FRGUI). 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/35392?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

35392, 1995-021F

Orbit

SSO

Country

ESA

Related business

European Space Agency (FR)

Manufacturer

Unknown

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1995-04-21 (31 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

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: 2 days ago

TLE from 2 days ago

0 ERS 2 DEB
1 35392U 95021F   26171.37210480  .00002038  00000-0  48811-3 0  9999
2 35392  98.3121 142.8689 0004515  90.8766 269.2948 14.54577145969688

Epoch: 2026-06-20T08:55Z

TLE epoch observation values (Epoch: 2026-06-20T08:55:49.854Z)

Latitude

-0.00005°

Longitude

100.32351°

Altitude

713.753 km

Speed

7.499 km/s

True Right ascension

09h 31m 28s

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

23:08:33

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

711.031 km

Perigee altitude

704.633 km

Semi-major axis

7,085.969 km

Eccentricity

0.00045

Inclination

98.3121°

RAAN

142.8689°

Arg. of periapsis

90.8766°

True anomaly

269.24307°

Mean anomaly

269.2948°

Eccentric anomaly

269.26893°

Mean motion

3.63868 °/min

Orbital period

98.94 mins

BSTAR

0.00048811

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Other satellites on launch #21 in the year 1995 (1995-04-21 UTC)

ERS 2 DEB, 31137

ARIANE 40+ DEB, 43351 (Decayed)

ERS 2 DEB, 28066 (Decayed)

ARIANE 40+ R/B, 23561

ERS 2 DEB, 35391

ERS 2 DEB, 35393

ERS 2 DEB, 44440 (Decayed)

ERS 2 DEB, 39478 (Decayed)

ERS 2, 23560 (Decayed)

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ERS 2 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 22:08:16.688Z	167.834° S	2026-06-22 22:12:16.688Z	326.818° NNW	44.306°	2026-06-22 22:16:16.688Z	345.82° N
6 mins	2026-06-23 10:10:16.688Z	48.903° ENE	2026-06-23 10:13:16.688Z	99.388° ESE	23.616°	2026-06-23 10:16:16.688Z	145.771° SSE
6 mins	2026-06-23 11:48:16.688Z	340.876° N	2026-06-23 11:51:16.688Z	283.354° WNW	27.362°	2026-06-23 11:54:16.688Z	235.594° 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 ERS 2 DEB, 35392 on other resources

View ERS 2 DEB, 35392 on Heavens-Above

View ERS 2 DEB, 35392 on Keep Track

View ERS 2 DEB, 35392 on Celestrak

View ERS 2 DEB, 35392 on Gunter's Space Page

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

ERS 2 DEB, 35392

Orbit data source: Space-Track

Expand to show TLE details & historyLast TLE update: 2 days ago

TLE from 2 days ago

TLE epoch observation values (Epoch: 2026-06-20T08:55:49.854Z)

Visualization orbit readout

Visualization observer readout

Orbital elements

Other satellites on launch #21 in the year 1995 (1995-04-21 UTC)

ERS 2 DEB Visibility forecast

Co-orbital & Co-planar RSOs

Check out ERS 2 DEB, 35392 on other resources

Documentation

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