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ARIANE 2 DEB, 27030

Orbit data source: Space-Track

ARIANE 2 DEB, 27030 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/27030?theme=dark&initialShowStats=false

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ISO8601 Format

Identifier

27030, 1989-006K

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, 0.4 m

Radar Cross Section

Medium (>0.1 m² and <1 m²)

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

TLE from 3 weeks ago

0 ARIANE 2 DEB
1 27030U 89006K   26091.89816419  .00000052  00000-0  13869-2 0  9995
2 27030   8.7219 348.0522 7101123 251.0188  24.5271  2.37452430208163

Epoch: 2026-04-01T21:33Z

TLE epoch observation values (Epoch: 2026-04-01T21:33:21.386Z)

Latitude

0.00024°

Longitude

-165.67769°

Altitude

8,919.618 km

Speed

5.942 km/s

True Right ascension

23h 11m 39s

True Declination

0° 00' 01"

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

21:38:56

Azimuth

Unknown

Elevation

Unknown

Doppler factor

Unknown

Orbital elements

Apogee altitude

34,216.587 km

Perigee altitude

503.231 km

Semi-major axis

23,738.046 km

Eccentricity

0.71011

Inclination

8.7219°

RAAN

348.0522°

Arg. of periapsis

251.0188°

True anomaly

108.60872°

Mean anomaly

24.5271°

Eccentric anomaly

59.63076°

Mean motion

0.59344 °/min

Orbital period

606.63 mins

BSTAR

0.0013869

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

ARIANE 2 DEB, 27043

ARIANE 2 DEB, 40785

ARIANE 2 DEB, 33569

ARIANE 2 DEB, 33581

ARIANE 2 DEB, 27039

ARIANE 2 DEB, 40784

ARIANE 2 DEB, 42484

ARIANE 2 DEB, 27044

ARIANE 2 DEB, 28570

ARIANE 2 DEB, 27650

ARIANE 2 DEB, 33551

ARIANE 2 DEB, 33548

ARIANE 2 DEB, 33567

ARIANE 2 DEB, 40788

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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.
473 mins	2026-04-19 14:48:32.600Z	107.426° ESE	2026-04-19 20:44:32.600Z	126.331° SE	31.305°	2026-04-19 22:41:32.600Z	115.595° 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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings

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Check out ARIANE 2 DEB, 27030 on other resources

View ARIANE 2 DEB, 27030 on Heavens-Above

View ARIANE 2 DEB, 27030 on Keep Track

View ARIANE 2 DEB, 27030 on Celestrak

View ARIANE 2 DEB, 27030 on Gunter's Space Page

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

Documentation

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