IRIDIUM 36

Satellite information

Favourite Embed

Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 36 at a glance.

Uptime

10199

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 36.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 36

International designator: 1997-056C

Object number (NORAD): 24967

Object ID (CCSDS): 24967

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.163 minutes

Inclination: 86.4011 deg

SMA: 7144.391 km

Apoapsis: 767.895 km

Periapsis: 764.616 km

RAAN: 142.1108 deg

Eccentricy: 0.00022951

Argument of periapsis: 90.8335 deg

Mean anomaly: 269.3126 deg

Mean motion: 14.37656 rev/day

Mean motion (dot): 0.00000385 rev/day2

B* drag term: 0.00012156691 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, 6:51 p.m. UTC

TLE line 0: 0 IRIDIUM 36

TLE line 1: 1 24967U 97056C 25241.78552956 .00000385 00000-0 12157-3 0 9991

TLE line 2: 2 24967 86.4011 142.1108 0002295 90.8335 269.3126 14.37656000462792

Live tracking on map

Real-time ground track for satellite IRIDIUM 36.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 36.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-06-05 23:53:43 0.0001554033 675.0 (m) DEBRIS
THORAD AGENA D DEB SSO 2025-04-13 23:49:34 0.001193203 184.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-03-23 23:52:03 0.0001274093 662.0 (m) DEBRIS
DMSP 5D-2 F13 DEB SSO 2024-12-24 06:22:14 0.0002078501 890.0 (m) DEBRIS
CZ-6A DEB LEO 2024-11-29 11:35:14 0.0001543883 154.0 (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 36 was lifted into orbit during the mission ‘Delta II | Iridium 34 to 37 & 19’, on board a Delta II space rocket.

The launch took place on Sept. 27, 1997, 1:23 a.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 34 to 37 & 19
Delta II | Iridium 34 to 37 & 19

Agency: N/A

Status: Launch Successful

Launch date: Sept. 27, 1997, 1:23 a.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.