IRIDIUM 920

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 920 at a glance.

Uptime

10385

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: 99.88 minutes

Inclination: 86.3975 deg

SMA: 7130.935 km

Apoapsis: 760.309 km

Periapsis: 745.291 km

RAAN: 138.9111 deg

Eccentricy: 0.001053

Argument of periapsis: 206.4229 deg

Mean anomaly: 153.6436 deg

Mean motion: 14.41727045 rev/day

Mean motion (dot): 0.00000829 rev/day2

B* drag term: 0.00024806 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 7:16 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 11, 2025, 9:57 p.m. UTC

TLE line 0: 0 IRIDIUM 920

TLE line 1: 1 24871U 97034C 25345.91509057 .00000829 00000-0 24806-3 0 9992

TLE line 2: 2 24871 86.3975 138.9111 0010530 206.4229 153.6436 14.41727045492187

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
COSMOS 397 DEB LEO 2025-12-02 07:26:49 0.008581815 43.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-11-16 11:55:01 0.0001161335 382.0 (m) DEBRIS
DMSP 5D-2 F9 DEB SSO 2025-08-24 03:05:41 0.01215587 66.0 (m) DEBRIS
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

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

...

Latest news about this satellite

There are no fresh news available about this satellite. Check back as we update our databases every day.


Newsletter sign-up

Weekly statistics, charts and insights to help you stay on top of the space industry.