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

10219

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: 1997-051AF

Object number (NORAD): 33862

Object ID (CCSDS): 33862

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 98.128 minutes

Inclination: 86.4048 deg

SMA: 7047.298 km

Apoapsis: 707.632 km

Periapsis: 630.695 km

RAAN: 80.578 deg

Eccentricy: 0.00545862

Argument of periapsis: 45.4047 deg

Mean anomaly: 77.5276 deg

Mean motion: 14.67468555 rev/day

Mean motion (dot): 0.00004578 rev/day2

B* drag term: 0.00078665653 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, 10:29 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 33862U 97051AF 25248.93730735 .00004578 00000-0 78666-3 0 9992

TLE line 2: 2 33862 86.4048 80.5780 0054586 45.4047 77.5276 14.67468555873883

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
COSMOS 2251 DEB LEO 2025-07-29 02:10:20 0.0001694143 111.0 (m) DEBRIS
CZ-6A DEB LEO 2025-02-27 18:10:32 0.0006270134 154.0 (m) DEBRIS
DELTA 1 DEB SSO 2024-11-12 00:59:08 0.0005742375 591.0 (m) DEBRIS
TIROS 4 LEO 2024-08-15 17:03:21 0.000216048 743.0 (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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