IRIDIUM 914

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 914 at a glance.

Uptime

10353

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 914.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 914

International designator: 1997-030A

Object number (NORAD): 24836

Object ID (CCSDS): 24836

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 99.931 minutes

Inclination: 86.3911 deg

SMA: 7133.365 km

Apoapsis: 757.361 km

Periapsis: 753.1 km

RAAN: 128.925 deg

Eccentricy: 0.0002987

Argument of periapsis: 117.924 deg

Mean anomaly: 242.2262 deg

Mean motion: 14.40990295 rev/day

Mean motion (dot): 0.00000743 rev/day2

B* drag term: 0.00022518 1/REarth

Two-line elements (TLE)

Creation date: Oct. 22, 2025, 12:06 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 21, 2025, 6:15 p.m. UTC

TLE line 0: 0 IRIDIUM 914

TLE line 1: 1 24836U 97030A 25294.76066810 .00000743 00000-0 22518-3 0 9993

TLE line 2: 2 24836 86.3911 128.9250 0002987 117.9240 242.2262 14.40990295625354

Live tracking on map

Real-time ground track for satellite IRIDIUM 914.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 914.

Target Orbit TCA Probability of collision Miss distance Type
COSMOS 2251 DEB LEO 2025-10-23 01:04:19 0.001007062 201.0 (m) DEBRIS
DMSP 5D-2 F11 DEB SSO 2025-09-14 19:18:08 0.000122032 208.0 (m) DEBRIS
CZ-6A DEB LEO 2025-08-24 10:45:38 0.0002994546 411.0 (m) DEBRIS
CZ-4 DEB SSO 2025-06-03 22:57:15 0.0009432369 755.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-12-15 13:52:33 0.0001257845 102.0 (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 914 was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 09 to 14 & Iridium 16’, on board a Proton-K/17S40 space rocket.

The launch took place on June 18, 1997, 2:02 p.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 09 to 14 & Iridium 16
Proton-K/17S40 | Iridium 09 to 14 & Iridium 16

Agency: N/A

Status: Launch Successful

Launch date: June 18, 1997, 2:02 p.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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