IRIDIUM 16

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 16 at a glance.

Uptime

10351

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 16.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 16

International designator: 1997-030F

Object number (NORAD): 24841

Object ID (CCSDS): 24841

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.082 minutes

Inclination: 86.4055 deg

SMA: 7140.552 km

Apoapsis: 764.944 km

Periapsis: 759.89 km

RAAN: 152.9426 deg

Eccentricy: 0.00035391

Argument of periapsis: 51.2347 deg

Mean anomaly: 308.9167 deg

Mean motion: 14.38815345 rev/day

Mean motion (dot): 0.00000574 rev/day2

B* drag term: 0.00018022199 1/REarth

Two-line elements (TLE)

Creation date: Oct. 20, 2025, 2:10 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 19, 2025, 9:27 p.m. UTC

TLE line 0: 0 IRIDIUM 16

TLE line 1: 1 24841U 97030F 25292.89402242 .00000574 00000-0 18022-3 0 9991

TLE line 2: 2 24841 86.4055 152.9426 0003539 51.2347 308.9167 14.38815345484934

Live tracking on map

Real-time ground track for satellite IRIDIUM 16.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 16.

Target Orbit TCA Probability of collision Miss distance Type
NOAA 16 DEB SSO 2025-09-22 19:17:49 0.005871 62.0 (m) DEBRIS
NOAA 16 DEB SSO 2025-09-17 22:59:06 0.0001066116 843.0 (m) DEBRIS
CZ-6A DEB SSO 2025-09-17 19:32:03 0.000893416 181.0 (m) DEBRIS
CZ-6A DEB SSO 2025-09-12 02:40:01 0.002180519 132.0 (m) DEBRIS
CZ-6A DEB SSO 2025-04-27 15:33:54 0.0001351963 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 16 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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