IRIDIUM 42

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 42 at a glance.

Uptime

10011

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 42.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 42

International designator: 1997-077A

Object number (NORAD): 25077

Object ID (CCSDS): 25077

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.256 minutes

Inclination: 86.3946 deg

SMA: 7148.825 km

Apoapsis: 771.755 km

Periapsis: 769.625 km

RAAN: 257.0935 deg

Eccentricy: 0.000149

Argument of periapsis: 103.2567 deg

Mean anomaly: 256.8796 deg

Mean motion: 14.36318451 rev/day

Mean motion (dot): 0.00000722 rev/day2

B* drag term: 0.00024051 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 7:38 p.m. UTC

TLE line 0: 0 IRIDIUM 42

TLE line 1: 1 25077U 97077A 25125.81833981 .00000722 00000-0 24051-3 0 9993

TLE line 2: 2 25077 86.3946 257.0935 0001490 103.2567 256.8796 14.36318451435111

Live tracking on map

Real-time ground track for satellite IRIDIUM 42.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 42.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-03-29 15:13:54 0.0002367582 463.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-12-20 05:02:39 0.0002229383 479.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-11-17 17:48:11 0.0001004061 597.0 (m) DEBRIS
DMSP 5D-2 F11 DEB SSO 2024-06-20 21:44:46 0.00015094 665.0 (m) DEBRIS

Associated space launch

Iridium provides global mobile telecommunications services using a constellation of 66 low earth orbit satellites in a 86.4° inclined orbit. Although 77 satellites were originally envisioned for the system and spawned the name based on the 77th element in the periodic table, the system has been scaled back. Motorola's Satellite Communications Group designed and manufactured the Iridium satellites with Lockheed Martin providing the LM-700A spacecraft buses.

IRIDIUM 42 was lifted into orbit during the mission ‘Long March 2C/SD | Iridium 42 & 44’, on board a Long March 2C/SD space rocket.

The launch took place on Dec. 8, 1997, 7:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 2C/SD | Iridium 42 & 44
Long March 2C/SD | Iridium 42 & 44

Agency: N/A

Status: Launch Successful

Launch date: Dec. 8, 1997, 7:16 a.m. UTC

Rocket: Long March 2C/SD

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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