IRIDIUM 33

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 33 at a glance.

Uptime

10212

Days in orbit

Revolutions

≈ 14.3

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 33.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 33

International designator: 1997-051C

Object number (NORAD): 24946

Object ID (CCSDS): 24946

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.353 minutes

Inclination: 86.3852 deg

SMA: 7153.437 km

Apoapsis: 780.542 km

Periapsis: 770.062 km

RAAN: 112.339 deg

Eccentricy: 0.00073249

Argument of periapsis: 183.1666 deg

Mean anomaly: 176.9485 deg

Mean motion: 14.34929773 rev/day

Mean motion (dot): 0.00000262 rev/day2

B* drag term: 0.000085161559 1/REarth

Two-line elements (TLE)

Creation date: Aug. 30, 2025, 3:38 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 29, 2025, 4:34 p.m. UTC

TLE line 0: 0 IRIDIUM 33

TLE line 1: 1 24946U 97051C 25241.69084667 .00000262 00000-0 85162-4 0 9993

TLE line 2: 2 24946 86.3852 112.3390 0007325 183.1666 176.9485 14.34929773463288

Live tracking on map

Real-time ground track for satellite IRIDIUM 33.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 33.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-08-28 23:19:33 0.0002541188 357.0 (m) DEBRIS
COSMOS 1371 LEO 2025-05-04 20:02:53 0.001110008 502.0 (m) PAYLOAD
DMSP 5D-2 F13 DEB SSO 2025-01-06 02:34:44 0.001245541 111.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-19 08:17:09 0.0002456107 640.0 (m) DEBRIS
COSMOS 1275 DEB LEO 2024-12-17 10:21:53 0.0001009904 458.0 (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 33 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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