IRIDIUM 911

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 911 at a glance.

Uptime

10185

Days in orbit

Revolutions

≈ 14.5

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 911.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 911

International designator: 1997-030G

Object number (NORAD): 24842

Object ID (CCSDS): 24842

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.475 minutes

Inclination: 86.4498 deg

SMA: 7111.645 km

Apoapsis: 742.423 km

Periapsis: 724.597 km

RAAN: 221.467 deg

Eccentricy: 0.0012533

Argument of periapsis: 229.2745 deg

Mean anomaly: 130.737 deg

Mean motion: 14.4759701 rev/day

Mean motion (dot): 0.00000789 rev/day2

B* drag term: 0.00020889 1/REarth

Two-line elements (TLE)

Creation date: May 7, 2025, 3:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 6, 2025, 6:44 p.m. UTC

TLE line 0: 0 IRIDIUM 911

TLE line 1: 1 24842U 97030G 25126.78083485 .00000789 00000-0 20889-3 0 9992

TLE line 2: 2 24842 86.4498 221.4670 0012533 229.2745 130.7370 14.47597010469095

Live tracking on map

Real-time ground track for satellite IRIDIUM 911.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 911.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-03-15 07:55:50 0.0003487983 848.0 (m) DEBRIS
DMSP 5D-2 F15 DEB SSO 2025-01-25 00:51:15 0.0002190726 648.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-01-05 14:32:23 0.00394561 132.0 (m) DEBRIS
SL-12 DEB LEO 2025-01-01 06:12:08 0.0003695267 416.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-26 00:35:13 0.0001426727 770.0 (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 911 was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 09 to 14 & Iridium 16’, on board a Proton-K/17S40 space rocket.

The launch took place on June 18, 1997, 2:02 p.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 09 to 14 & Iridium 16
Proton-K/17S40 | Iridium 09 to 14 & Iridium 16

Agency: N/A

Status: Launch Successful

Launch date: June 18, 1997, 2:02 p.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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