IRIDIUM 29

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 29 at a glance.

Uptime

10156

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 29.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 29

International designator: 1997-051A

Object number (NORAD): 24944

Object ID (CCSDS): 24944

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.245 minutes

Inclination: 86.3979 deg

SMA: 7148.292 km

Apoapsis: 771.678 km

Periapsis: 768.635 km

RAAN: 136.6746 deg

Eccentricy: 0.0002129

Argument of periapsis: 89.749 deg

Mean anomaly: 270.3951 deg

Mean motion: 14.36479316 rev/day

Mean motion (dot): 0.00000343 rev/day2

B* drag term: 0.00011036 1/REarth

Two-line elements (TLE)

Creation date: July 4, 2025, 6:39 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 4, 2025, 9:56 a.m. UTC

TLE line 0: 0 IRIDIUM 29

TLE line 1: 1 24944U 97051A 25185.41431919 .00000343 00000-0 11036-3 0 9992

TLE line 2: 2 24944 86.3979 136.6746 0002129 89.7490 270.3951 14.36479316455747

Live tracking on map

Real-time ground track for satellite IRIDIUM 29.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 29.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-04-24 00:05:05 0.0006978004 234.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-07 10:49:56 0.0007198399 110.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-02-25 16:14:02 0.0003546407 526.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-17 01:19:38 0.004126419 140.0 (m) DEBRIS
DELTA 1 DEB SSO 2025-01-12 13:31:49 0.001092307 179.0 (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 29 was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 27 to 33’, on board a Proton-K/17S40 space rocket.

The launch took place on Sept. 14, 1997, 1:36 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 27 to 33
Proton-K/17S40 | Iridium 27 to 33

Agency: N/A

Status: Launch Successful

Launch date: Sept. 14, 1997, 1:36 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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