IRIDIUM 44

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 44 at a glance.

Uptime

10011

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 44.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 44

International designator: 1997-077B

Object number (NORAD): 25078

Object ID (CCSDS): 25078

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.986 minutes

Inclination: 86.3973 deg

SMA: 7135.949 km

Apoapsis: 760.159 km

Periapsis: 755.47 km

RAAN: 239.1234 deg

Eccentricy: 0.0003286

Argument of periapsis: 128.389 deg

Mean anomaly: 231.7605 deg

Mean motion: 14.40207648 rev/day

Mean motion (dot): 0.00000637 rev/day2

B* drag term: 0.00019522 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, 7:37 p.m. UTC

TLE line 0: 0 IRIDIUM 44

TLE line 1: 1 25078U 97077B 25125.81764036 .00000637 00000-0 19522-3 0 9990

TLE line 2: 2 25078 86.3973 239.1234 0003286 128.3890 231.7605 14.40207648437604

Live tracking on map

Real-time ground track for satellite IRIDIUM 44.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 44.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-03-15 05:05:31 0.0002798018 77.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2025-02-22 02:36:20 0.0001437179 639.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-31 18:21:13 0.0001021112 41.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-09-27 00:40:22 0.0002964015 229.0 (m) DEBRIS
NOAA 17 DEB SSO 2024-08-08 02:11:36 0.0002016205 617.0 (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 44 was lifted into orbit during the mission ‘Long March 2C/SD | Iridium 42 & 44’, on board a Long March 2C/SD space rocket.

The launch took place on Dec. 8, 1997, 7:16 a.m. from Launch Complex 7.

For more information about the launch, click the button.

Launch to space Long March 2C/SD | Iridium 42 & 44
Long March 2C/SD | Iridium 42 & 44

Agency: N/A

Status: Launch Successful

Launch date: Dec. 8, 1997, 7:16 a.m. UTC

Rocket: Long March 2C/SD

Launch pad: Launch Complex 7

Location: Taiyuan Satellite Launch Center, People's Republic of China

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