IRIDIUM 28

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 28 at a glance.

Uptime

10096

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 28.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 28

International designator: 1997-051E

Object number (NORAD): 24948

Object ID (CCSDS): 24948

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.184 minutes

Inclination: 86.3981 deg

SMA: 7145.382 km

Apoapsis: 768.698 km

Periapsis: 765.795 km

RAAN: 159.2191 deg

Eccentricy: 0.0002032

Argument of periapsis: 101.5638 deg

Mean anomaly: 258.5788 deg

Mean motion: 14.37356938 rev/day

Mean motion (dot): 0.00000474 rev/day2

B* drag term: 0.00015213 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, 6:52 p.m. UTC

TLE line 0: 0 IRIDIUM 28

TLE line 1: 1 24948U 97051E 25125.78644267 .00000474 00000-0 15213-3 0 9998

TLE line 2: 2 24948 86.3981 159.2191 0002032 101.5638 258.5788 14.37356938447752

Live tracking on map

Real-time ground track for satellite IRIDIUM 28.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 28.

Target Orbit TCA Probability of collision Miss distance Type
FENGYUN 1C DEB SSO 2025-04-20 01:01:10 0.0002838781 910.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-02-13 03:19:19 0.0003478477 685.0 (m) DEBRIS
COSMOS 1867 COOLANT LEO 2024-12-24 03:12:36 0.0003481297 754.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-10-14 09:25:34 0.0006793494 69.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-06-01 06:47:10 0.0002074072 81.0 (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 28 was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 27 to 33’, on board a Proton-K/17S40 space rocket.

The launch took place on Sept. 14, 1997, 1:36 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 27 to 33
Proton-K/17S40 | Iridium 27 to 33

Agency: N/A

Status: Launch Successful

Launch date: Sept. 14, 1997, 1:36 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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