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

11960

Days in orbit

Revolutions

≈ 12.4

Per day

Orbit

HEO

HEO

Inclination

65.8

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: 1992-052P

Object number (NORAD): 47108

Object ID (CCSDS): 47108

Country: FRANCE (FR)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 115.835 minutes

Inclination: 65.8153 deg

SMA: 7871.439 km

Apoapsis: 2410.864 km

Periapsis: 575.743 km

RAAN: 114.1989 deg

Eccentricy: 0.1165683

Argument of periapsis: 90.887 deg

Mean anomaly: 282.5571 deg

Mean motion: 12.4314445 rev/day

Mean motion (dot): 0.00001968 rev/day2

B* drag term: 0.0011063 1/REarth

Two-line elements (TLE)

Creation date: May 7, 2025, 3:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 6, 2025, 5:20 a.m. UTC

TLE line 0: 0 ARIANE 42P DEB *

TLE line 1: 1 47108U 92052P 25126.22252518 .00001968 00000-0 11063-2 0 9998

TLE line 2: 2 47108 65.8153 114.1989 1165683 90.8870 282.5571 12.43144450 48599

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
TIROS 4 LEO 2025-02-11 23:19:07 0.0006865494 797.0 (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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