IRIDIUM 71

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 71 at a glance.

Uptime

9865

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 71.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 71

International designator: 1998-026B

Object number (NORAD): 25320

Object ID (CCSDS): 25320

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.922 minutes

Inclination: 86.3933 deg

SMA: 7132.937 km

Apoapsis: 755.878 km

Periapsis: 753.725 km

RAAN: 108.4261 deg

Eccentricy: 0.0001509

Argument of periapsis: 152.6459 deg

Mean anomaly: 207.4821 deg

Mean motion: 14.41120158 rev/day

Mean motion (dot): 0.00000746 rev/day2

B* drag term: 0.0002256 1/REarth

Two-line elements (TLE)

Creation date: May 5, 2025, 2:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 4, 2025, 8:56 p.m. UTC

TLE line 0: 0 IRIDIUM 71

TLE line 1: 1 25320U 98026B 25124.87242520 .00000746 00000-0 22560-3 0 9996

TLE line 2: 2 25320 86.3933 108.4261 0001509 152.6459 207.4821 14.41120158417356

Live tracking on map

Real-time ground track for satellite IRIDIUM 71.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 71.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-01-25 13:05:35 0.0005566703 725.0 (m) DEBRIS
NOAA 17 DEB SSO 2024-12-17 17:38:25 0.0001417571 624.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-03 04:09:59 0.0002594318 229.0 (m) DEBRIS
DELTA 1 DEB LEO 2024-07-16 17:34:48 0.0003390527 991.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-06-23 01:18:41 0.0001013824 920.0 (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 71 was lifted into orbit during the mission ‘Long March 2C/SD | Iridium 69 & 71’, on board a Long March 2C/SD space rocket.

The launch took place on May 2, 1998, 9:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 2C/SD | Iridium 69 & 71
Long March 2C/SD | Iridium 69 & 71

Agency: N/A

Status: Launch Successful

Launch date: May 2, 1998, 9:16 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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