IRIDIUM 33 DEB

Satellite information

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Satellite Type and Status

DEBRISIN ORBIT

Key statistics

Satellite IRIDIUM 33 DEB at a glance.

Uptime

10266

Days in orbit

Revolutions

≈ 14.7

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.4

Latest

Satellite identification and parameters

Extended collection of information and parameters for IRIDIUM 33 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 33 DEB

International designator: 1997-051WG

Object number (NORAD): 36490

Object ID (CCSDS): 36490

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.659 minutes

Inclination: 86.3687 deg

SMA: 7024.817 km

Apoapsis: 648.574 km

Periapsis: 644.791 km

RAAN: 33.9581 deg

Eccentricy: 0.0002693

Argument of periapsis: 219.7472 deg

Mean anomaly: 140.3549 deg

Mean motion: 14.74518411 rev/day

Mean motion (dot): 0.00019047 rev/day2

B* drag term: 0.0028555 1/REarth

Two-line elements (TLE)

Creation date: Oct. 21, 2025, 11:56 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 21, 2025, 1:17 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 36490U 97051WG 25294.55391183 .00019047 00000-0 28555-2 0 9999

TLE line 2: 2 36490 86.3687 33.9581 0002693 219.7472 140.3549 14.74518411857151

Live tracking on map

Real-time ground track for satellite IRIDIUM 33 DEB.

In-orbit conjunctions

A list of the most updated potential collisions computed for object IRIDIUM 33 DEB.

Target Orbit TCA Probability of collision Miss distance Type
RUBIN 2 LEO 2025-05-16 16:14:26 0.0008085514 145.0 (m) PAYLOAD
CZ-6A DEB LEO 2025-04-07 19:21:22 0.0001144173 46.0 (m) DEBRIS
CZ-4B DEB SSO 2024-08-26 15:22:53 0.0006233529 57.0 (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 33 DEB 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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