ARIANE 2 DEB, 26727

Orbit data source: Space-Track

ARIANE 2 DEB, 26727 is space debris in HEO originally from a launch on Fri, 27 Jan 1989 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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https://www.satcat.com/sats-embedded/26727?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

26727, 1989-006E

Orbit

HEO

Country

FR

Related business

ArianeGroup (FR)

Manufacturer

EADS/LV

Mission

Spacecraft

Bus & Motor

Unknown

Mass

Unknown

Launch date (UTC)

1989-01-27 (37 years ago)

Launch vehicle

Unknown

Launch site

French Guiana (FRGUI)

Object type

Payload

Rocket body

Debris

Shape & HBR

Unknown shape, 0.3 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 18 hours ago

TLE from 18 hours ago

0 ARIANE 2 DEB
1 26727U 89006E   25348.87459712  .00000091  00000-0  15909-2 0  9998
2 26727   7.7920 168.9640 7159779 253.1057  28.1298  2.28903076207470

Epoch: 2025-12-14T20:59Z

TLE epoch observation values (Epoch: 2025-12-14T20:59:25.191Z)

Latitude

1.14735°

Longitude

138.71271°

Altitude

10,674.529 km

Speed

5.51 km/s

True Right ascension

11h 49m 23s

True Declination

1° 08' 40"

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

13:22:51

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

35,363.724 km

Perigee altitude

530.816 km

Semi-major axis

24,325.407 km

Eccentricity

0.71598

Inclination

7.792°

RAAN

168.964°

Arg. of periapsis

253.1057°

True anomaly

115.31502°

Mean anomaly

28.1298°

Eccentric anomaly

65.44123°

Mean motion

0.57208 °/min

Orbital period

629.29 mins

BSTAR

0.0015909

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Other satellites on launch #6 in the year 1989 (1989-01-27 UTC)

ARIANE 2 DEB, 42485

ARIANE 2 DEB, 27602

ARIANE 2 DEB, 27042

ARIANE 2 DEB, 28567

INTELSAT 515, 19772

ARIANE 2 DEB, 40784

ARIANE 2 DEB, 28565

ARIANE 2 DEB, 42483

ARIANE 2 DEB, 40787

ARIANE 2 DEB, 33579

ARIANE 2 DEB, 33578

ARIANE 2 DEB, 33556

ARIANE 2 DEB, 26726

ARIANE 2 DEB, 27033

ARIANE 2 DEB, 27034

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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.

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ARIANE 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.
215 mins	2025-12-15 18:34:17.616Z	252.794° W	2025-12-15 19:52:17.616Z	253.445° W	16.877°	2025-12-15 22:09:17.616Z	263.789° W

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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 ARIANE 2 DEB, 26727 on other resources

View ARIANE 2 DEB, 26727 on Heavens-Above

View ARIANE 2 DEB, 26727 on Keep Track

View ARIANE 2 DEB, 26727 on Celestrak

View ARIANE 2 DEB, 26727 on Gunter's Space Page

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

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