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

10220

Days in orbit

Revolutions

≈ 14.8

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: 1997-051QJ

Object number (NORAD): 35488

Object ID (CCSDS): 35488

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.269 minutes

Inclination: 86.3335 deg

SMA: 7006.106 km

Apoapsis: 647.924 km

Periapsis: 608.018 km

RAAN: 345.9358 deg

Eccentricy: 0.00284795

Argument of periapsis: 26.7117 deg

Mean anomaly: 333.5564 deg

Mean motion: 14.80429512 rev/day

Mean motion (dot): 0.00013241 rev/day2

B* drag term: 0.0017164879 1/REarth

Two-line elements (TLE)

Creation date: Sept. 6, 2025, 2:09 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Sept. 5, 2025, 6:03 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35488U 97051QJ 25248.75215675 .00013241 00000-0 17165-2 0 9992

TLE line 2: 2 35488 86.3335 345.9358 0028480 26.7117 333.5564 14.80429512868154

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
FENGYUN 1C DEB SSO 2025-03-06 08:05:44 0.0002264361 18.0 (m) DEBRIS
TIROS 4 LEO 2024-09-09 15:35:24 0.0002202469 174.0 (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 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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