ARIANE 42P DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite ARIANE 42P DEB at a glance.

Uptime

12083

Days in orbit

Revolutions

≈ 12.9

Per day

Orbit

LEO

Low Earth Orbit

Inclination

65.9

Latest

Satellite identification and parameters

Extended collection of information and parameters for ARIANE 42P DEB.

Object identification

Identified? True

Debris? True

Object name: ARIANE 42P DEB

International designator: 1992-052K

Object number (NORAD): 44512

Object ID (CCSDS): 44512

Country: FRANCE (FR)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 111.977 minutes

Inclination: 65.9133 deg

SMA: 7695.646 km

Apoapsis: 1508.461 km

Periapsis: 1126.561 km

RAAN: 103.6339 deg

Eccentricy: 0.02481277

Argument of periapsis: 86.9095 deg

Mean anomaly: 276.028 deg

Mean motion: 12.85982688 rev/day

Mean motion (dot): 0.00002732 rev/day2

B* drag term: 0.0098881156 1/REarth

Two-line elements (TLE)

Creation date: Sept. 7, 2025, 3:09 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 6, 2025, 8:54 p.m. UTC

TLE line 0: 0 ARIANE 42P DEB

TLE line 1: 1 44512U 92052K 25249.87137994 .00002732 00000-0 98881-2 0 9994

TLE line 2: 2 44512 65.9133 103.6339 0248128 86.9095 276.0280 12.85982688283939

Live tracking on map

Real-time ground track for satellite ARIANE 42P DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object ARIANE 42P DEB.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 877 LEO 2025-01-23 13:52:58 0.0001270594 158.0 (m) PAYLOAD

Associated space launch

The TOPEX/POSEIDON satellite was launched on 10 August 1992 with the objective of "observing and understanding the ocean circulation". A joint project between NASA, the U.S. space agency, and CNES, the French space agency, it carries two radar altimeters and precise orbit determination systems, including the DORIS system. KITSAT-1 (Korean Institute of Technology Satellite) was a collaborative research mission, encompassing the installation of a groundstation in South Korea, participation of Korean engineers in the UoSAT-5 mission, technology transfer and training of students on the MSc courses at Surrey, and the involvement in a engineering and flight microsatellites. The S80/T satellite was built for CNES by Matra Marconi Space using the Surrey Satellite Technology Microbus (Uosat) bus.

ARIANE 42P DEB was lifted into orbit during the mission ‘Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T’, on board a Ariane 42P space rocket.

The launch took place on Aug. 10, 1992, 11:08 p.m. from Ariane Launch Area 2.

For more information about the launch, click the button.

Launch to space Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T
Ariane 42P | Topex-Poseidon, Kitsat 1 & S80/T

Agency: N/A

Status: Launch Successful

Launch date: Aug. 10, 1992, 11:08 p.m. UTC

Rocket: Ariane 42P

Launch pad: Ariane Launch Area 2

Location: Guiana Space Centre, French Guiana

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