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

10158

Days in orbit

Revolutions

≈ 14.4

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.3

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: 1997-051YJ

Object number (NORAD): 38022

Object ID (CCSDS): 38022

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.008 minutes

Inclination: 86.2676 deg

SMA: 7137.014 km

Apoapsis: 789.858 km

Periapsis: 727.9 km

RAAN: 86.544 deg

Eccentricy: 0.0043406

Argument of periapsis: 212.6554 deg

Mean anomaly: 147.196 deg

Mean motion: 14.39885393 rev/day

Mean motion (dot): 0.00002026 rev/day2

B* drag term: 0.00063203 1/REarth

Two-line elements (TLE)

Creation date: July 5, 2025, 5:45 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 5, 2025, 10:46 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 38022U 97051YJ 25186.44877804 .00002026 00000-0 63203-3 0 9998

TLE line 2: 2 38022 86.2676 86.5440 0043406 212.6554 147.1960 14.39885393668866

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
SL-8 R/B LEO 2025-04-27 07:38:49 0.0001476629 743.0 (m) ROCKET BODY
CZ-6A DEB LEO 2025-02-02 01:09:08 0.0001623564 157.0 (m) DEBRIS
CZ-6A DEB LEO 2025-01-23 05:41:13 0.0001453249 293.0 (m) DEBRIS
CZ-6A DEB LEO 2024-10-14 04:19:53 0.0004792615 265.0 (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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