IRIDIUM 63

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite IRIDIUM 63 at a glance.

Uptime

10112

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 63.

Object identification

Identified? True

Debris? False

Object name: IRIDIUM 63

International designator: 1998-021B

Object number (NORAD): 25286

Object ID (CCSDS): 25286

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: LARGE

Orbital parameters

Period: 100.227 minutes

Inclination: 86.3984 deg

SMA: 7147.443 km

Apoapsis: 771.029 km

Periapsis: 767.588 km

RAAN: 7.4664 deg

Eccentricy: 0.0002407

Argument of periapsis: 89.3164 deg

Mean anomaly: 270.8309 deg

Mean motion: 14.36734999 rev/day

Mean motion (dot): 0.00000587 rev/day2

B* drag term: 0.00019249718 1/REarth

Two-line elements (TLE)

Creation date: Dec. 12, 2025, 10:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 12, 2025, 3:21 a.m. UTC

TLE line 0: 0 IRIDIUM 63

TLE line 1: 1 25286U 98021B 25346.13960580 .00000587 00000-0 19250-3 0 9995

TLE line 2: 2 25286 86.3984 7.4664 0002407 89.3164 270.8309 14.36734999449397

Live tracking on map

Real-time ground track for satellite IRIDIUM 63.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 63.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB LEO 2025-11-07 06:19:32 0.0002395694 345.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-11-01 23:19:47 0.0001089081 456.0 (m) DEBRIS
COSMOS 1275 DEB LEO 2025-10-01 19:59:02 0.0001033516 403.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2025-07-01 04:00:16 0.0006950139 178.0 (m) DEBRIS
COSMOS 1110 LEO 2025-06-29 16:52:40 0.0001229858 445.0 (m) PAYLOAD

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 63 was lifted into orbit during the mission ‘Proton-K/17S40 | Iridium 62 to 68’, on board a Proton-K/17S40 space rocket.

The launch took place on April 7, 1998, 2:13 a.m. from 81/23 (81L).

For more information about the launch, click the button.

Launch to space Proton-K/17S40 | Iridium 62 to 68
Proton-K/17S40 | Iridium 62 to 68

Agency: N/A

Status: Launch Successful

Launch date: April 7, 1998, 2:13 a.m. UTC

Rocket: Proton-K/17S40

Launch pad: 81/23 (81L)

Location: Baikonur Cosmodrome, Republic of Kazakhstan

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