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

10157

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: 100.207 minutes

Inclination: 86.375 deg

SMA: 7146.49 km

Apoapsis: 815.16 km

Periapsis: 721.551 km

RAAN: 170.4399 deg

Eccentricy: 0.0065493

Argument of periapsis: 341.7141 deg

Mean anomaly: 18.1701 deg

Mean motion: 14.37022443 rev/day

Mean motion (dot): 0.00002774 rev/day2

B* drag term: 0.00090699 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, 10:44 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34508U 97051GZ 25186.44741893 .00002774 00000-0 90699-3 0 9990

TLE line 2: 2 34508 86.3750 170.4399 0065493 341.7141 18.1701 14.37022443850069

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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