IRIDIUM 4

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 4 at a glance.

Uptime

10344

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 4.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 4

International designator: 1997-020E

Object number (NORAD): 24796

Object ID (CCSDS): 24796

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.217 minutes

Inclination: 86.4002 deg

SMA: 7146.944 km

Apoapsis: 770.258 km

Periapsis: 767.361 km

RAAN: 142.9121 deg

Eccentricy: 0.00020268

Argument of periapsis: 84.0741 deg

Mean anomaly: 276.0687 deg

Mean motion: 14.36885469 rev/day

Mean motion (dot): 0.00000402 rev/day2

B* drag term: 0.0001294631 1/REarth

Two-line elements (TLE)

Creation date: Aug. 30, 2025, 3:38 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 29, 2025, 8:09 p.m. UTC

TLE line 0: 0 IRIDIUM 4

TLE line 1: 1 24796U 97020E 25241.84018819 .00000402 00000-0 12946-3 0 9990

TLE line 2: 2 24796 86.4002 142.9121 0002027 84.0741 276.0687 14.36885469483044

Live tracking on map

Real-time ground track for satellite IRIDIUM 4.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 4.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-08-07 12:52:38 0.0002953508 614.0 (m) DEBRIS
CZ-6A DEB LEO 2025-05-24 04:30:23 0.0001070858 854.0 (m) DEBRIS
COSMOS 676 LEO 2025-02-11 00:29:36 0.0003113934 169.0 (m) PAYLOAD
COSMOS 1818 COOLANT LEO 2024-12-19 23:41:05 0.0004949293 922.0 (m) DEBRIS
RESURS O1 DEB SSO 2024-09-06 07:27:54 0.001060241 262.0 (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 4 was lifted into orbit during the mission ‘Delta II | Iridium 04 to 08’, on board a Delta II space rocket.

The launch took place on May 5, 1997, 2:55 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 04 to 08
Delta II | Iridium 04 to 08

Agency: N/A

Status: Launch Successful

Launch date: May 5, 1997, 2:55 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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