ERS 2 DEB, 35391

Orbit data source: Space-Track

ERS 2 DEB, 35391 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/35391?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

35391, 1995-021E

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: 3 days ago

TLE from 3 days ago

0 ERS 2 DEB
1 35391U 95021E   26170.91530003  .00001460  00000-0  39557-3 0  9998
2 35391  98.6150 154.2695 0006760 101.2988 288.1386 14.49182880998087

Epoch: 2026-06-19T21:58Z

TLE epoch observation values (Epoch: 2026-06-19T21:58:01.922Z)

Latitude

29.04913°

Longitude

-88.17715°

Altitude

730.457 km

Speed

7.493 km/s

True Right ascension

09h 57m 52s

True Declination

28° 54' 10"

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

23:08:14

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

730.236 km

Perigee altitude

720.632 km

Semi-major axis

7,103.571 km

Eccentricity

0.00068

Inclination

98.615°

RAAN

154.2695°

Arg. of periapsis

101.2988°

True anomaly

288.06497°

Mean anomaly

288.1386°

Eccentric anomaly

288.10179°

Mean motion

3.62517 °/min

Orbital period

99.31 mins

BSTAR

0.00039557

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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, 35392

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.
9 mins	2026-06-22 22:50:57.386Z	164.661° S	2026-06-22 22:55:57.386Z	354.415° N	44.75°	2026-06-22 22:59:57.386Z	346.874° N
6 mins	2026-06-23 10:56:57.386Z	52.925° ENE	2026-06-23 10:59:57.386Z	104.035° ESE	22.806°	2026-06-23 11:02:57.386Z	146.622° SSE

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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, 35391 on other resources

View ERS 2 DEB, 35391 on Heavens-Above

View ERS 2 DEB, 35391 on Keep Track

View ERS 2 DEB, 35391 on Celestrak

View ERS 2 DEB, 35391 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, 35391

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: 2026-06-19T21:58:01.922Z)

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, 35391 on other resources

Documentation

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