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

10212

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 33 DEB.

Object identification

Identified? True

Debris? True

Object name: IRIDIUM 33 DEB

International designator: 1997-051GZ

Object number (NORAD): 34508

Object ID (CCSDS): 34508

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.187 minutes

Inclination: 86.3757 deg

SMA: 7145.536 km

Apoapsis: 814.174 km

Periapsis: 720.628 km

RAAN: 147.0977 deg

Eccentricy: 0.00654578

Argument of periapsis: 155.3451 deg

Mean anomaly: 205.0901 deg

Mean motion: 14.37310366 rev/day

Mean motion (dot): 0.00003507 rev/day2

B* drag term: 0.0011412552 1/REarth

Two-line elements (TLE)

Creation date: Aug. 30, 2025, 3:38 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 29, 2025, 5:31 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34508U 97051GZ 25241.73014504 .00003507 00000-0 11413-2 0 9997

TLE line 2: 2 34508 86.3757 147.0977 0065458 155.3451 205.0901 14.37310366858007

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
CZ-6A DEB LEO 2025-04-22 08:46:08 0.0001291204 103.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-11-15 09:16:40 0.0007411585 166.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-09-25 08:29:03 0.0003006285 224.0 (m) DEBRIS
PICOSAT 9 LEO 2024-09-15 17:22:15 0.0001203135 103.0 (m) PAYLOAD
COSMOS 2251 DEB LEO 2024-06-16 05:01:46 0.0001075252 300.0 (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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