IRIDIUM 38

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 38 at a glance.

Uptime

10040

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 38.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 38

International designator: 1997-069E

Object number (NORAD): 25043

Object ID (CCSDS): 25043

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.134 minutes

Inclination: 86.395 deg

SMA: 7142.989 km

Apoapsis: 765.729 km

Periapsis: 763.98 km

RAAN: 251.3929 deg

Eccentricy: 0.0001224

Argument of periapsis: 156.6114 deg

Mean anomaly: 203.514 deg

Mean motion: 14.38079039 rev/day

Mean motion (dot): 0.00000824 rev/day2

B* drag term: 0.00026567 1/REarth

Two-line elements (TLE)

Creation date: May 5, 2025, 2:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 4, 2025, 7:41 p.m. UTC

TLE line 0: 0 IRIDIUM 38

TLE line 1: 1 25043U 97069E 25124.82035604 .00000824 00000-0 26567-3 0 9990

TLE line 2: 2 25043 86.3950 251.3929 0001224 156.6114 203.5140 14.38079039439725

Live tracking on map

Real-time ground track for satellite IRIDIUM 38.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 38.

Target Orbit TCA Probability of collision Miss distance Type
DELTA 1 DEB SSO 2025-04-14 23:09:09 0.0002708334 165.0 (m) DEBRIS
SL-16 DEB LEO 2025-03-23 23:42:02 0.0001846849 261.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-03-02 06:29:29 0.0004539319 773.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-08 19:07:38 0.0001109983 382.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-10-21 12:39:45 0.0002697452 886.0 (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 38 was lifted into orbit during the mission ‘Delta II | Iridium 38 to 43’, on board a Delta II space rocket.

The launch took place on Nov. 9, 1997, 1:34 a.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 38 to 43
Delta II | Iridium 38 to 43

Agency: N/A

Status: Launch Successful

Launch date: Nov. 9, 1997, 1:34 a.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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