IRIDIUM 73

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 73 at a glance.

Uptime

9851

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 73.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 73

International designator: 1998-032C

Object number (NORAD): 25344

Object ID (CCSDS): 25344

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.196 minutes

Inclination: 86.4414 deg

SMA: 7098.353 km

Apoapsis: 722.231 km

Periapsis: 718.204 km

RAAN: 64.7818 deg

Eccentricy: 0.0002837

Argument of periapsis: 96.7441 deg

Mean anomaly: 263.4088 deg

Mean motion: 14.51665007 rev/day

Mean motion (dot): 0.00000986 rev/day2

B* drag term: 0.0002408 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 9:02 p.m. UTC

TLE line 0: 0 IRIDIUM 73

TLE line 1: 1 25344U 98032C 25125.87708045 .00000986 00000-0 24080-3 0 9994

TLE line 2: 2 25344 86.4414 64.7818 0002837 96.7441 263.4088 14.51665007424424

Live tracking on map

Real-time ground track for satellite IRIDIUM 73.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 73.

Target Orbit TCA Probability of collision Miss distance Type
IRIDIUM 33 DEB LEO 2024-11-02 11:16:33 0.0001437244 250.0 (m) DEBRIS
CZ-6A DEB SSO 2024-11-01 00:36:30 0.0001373345 384.0 (m) DEBRIS
IRIDIUM 33 DEB LEO 2024-10-31 07:08:37 0.0001913956 822.0 (m) DEBRIS
CZ-6A DEB SSO 2024-10-26 22:07:56 0.0001166649 81.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-08-21 12:52:48 0.0002369129 525.0 (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 73 was lifted into orbit during the mission ‘Delta II | Iridium 70, 72 to 75’, on board a Delta II space rocket.

The launch took place on May 17, 1998, 9:16 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 70, 72 to 75
Delta II | Iridium 70, 72 to 75

Agency: N/A

Status: Launch Successful

Launch date: May 17, 1998, 9:16 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

...

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