IRIDIUM 920

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 920 at a glance.

Uptime

10163

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 920.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 920

International designator: 1997-034C

Object number (NORAD): 24871

Object ID (CCSDS): 24871

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.896 minutes

Inclination: 86.3999 deg

SMA: 7131.688 km

Apoapsis: 760.978 km

Periapsis: 746.127 km

RAAN: 231.8869 deg

Eccentricy: 0.0010412

Argument of periapsis: 211.9389 deg

Mean anomaly: 148.1181 deg

Mean motion: 14.41498816 rev/day

Mean motion (dot): 0.00000662 rev/day2

B* drag term: 0.00019785 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, 7:27 p.m. UTC

TLE line 0: 0 IRIDIUM 920

TLE line 1: 1 24871U 97034C 25125.81058156 .00000662 00000-0 19785-3 0 9991

TLE line 2: 2 24871 86.3999 231.8869 0010412 211.9389 148.1181 14.41498816460477

Live tracking on map

Real-time ground track for satellite IRIDIUM 920.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 920.

Target Orbit TCA Probability of collision Miss distance Type
DMSP 5D-2 F13 DEB SSO 2025-04-29 12:18:27 0.000118208 660.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2025-02-25 20:35:40 0.0001554715 147.0 (m) DEBRIS
CZ-6A DEB LEO 2025-02-17 04:20:56 0.0001677629 961.0 (m) DEBRIS
FENGYUN 1C DEB * SSO 2025-02-10 07:29:09 0.0009828628 203.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-31 23:24:43 0.0005348044 177.0 (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 920 was lifted into orbit during the mission ‘Delta II | Iridium 15’, on board a Delta II space rocket.

The launch took place on July 9, 1997, 1:04 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 15
Delta II | Iridium 15

Agency: N/A

Status: Launch Successful

Launch date: July 9, 1997, 1:04 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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