IRIDIUM 17

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 17 at a glance.

Uptime

10281

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 17.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 17

International designator: 1997-034B

Object number (NORAD): 24870

Object ID (CCSDS): 24870

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.147 minutes

Inclination: 86.399 deg

SMA: 7143.643 km

Apoapsis: 768.117 km

Periapsis: 762.898 km

RAAN: 203.3613 deg

Eccentricy: 0.00036529

Argument of periapsis: 105.1537 deg

Mean anomaly: 255.0065 deg

Mean motion: 14.37881813 rev/day

Mean motion (dot): 0.00000766 rev/day2

B* drag term: 0.00024764784 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 8:28 p.m. UTC

TLE line 0: 0 IRIDIUM 17

TLE line 1: 1 24870U 97034B 25242.85322225 .00000766 00000-0 24765-3 0 9994

TLE line 2: 2 24870 86.3990 203.3613 0003653 105.1537 255.0065 14.37881813474311

Live tracking on map

Real-time ground track for satellite IRIDIUM 17.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 17.

Target Orbit TCA Probability of collision Miss distance Type
NOAA 17 DEB SSO 2025-08-20 17:09:22 0.0001212651 486.0 (m) DEBRIS
DELTA 1 DEB SSO 2025-04-23 07:38:31 0.0001336378 400.0 (m) DEBRIS
CZ-6A DEB SSO 2025-02-25 19:20:20 0.01221906 41.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-20 03:53:09 0.0007974429 520.0 (m) DEBRIS
NOAA 17 DEB SSO 2024-09-28 04:10:32 0.0001097544 954.0 (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 17 was lifted into orbit during the mission ‘Delta II | Iridium 15’, on board a Delta II space rocket.

The launch took place on July 9, 1997, 1:04 p.m. from Space Launch Complex 2W.

For more information about the launch, click the button.

Launch to space Delta II | Iridium 15
Delta II | Iridium 15

Agency: N/A

Status: Launch Successful

Launch date: July 9, 1997, 1:04 p.m. UTC

Rocket: Delta II

Launch pad: Space Launch Complex 2W

Location: Vandenberg SFB, CA, USA

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