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

≈ 14.2

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: 1997-051AK

Object number (NORAD): 33866

Object ID (CCSDS): 33866

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 101.065 minutes

Inclination: 86.3031 deg

SMA: 7187.227 km

Apoapsis: 890.515 km

Periapsis: 727.668 km

RAAN: 134.3818 deg

Eccentricy: 0.01132891

Argument of periapsis: 113.851 deg

Mean anomaly: 267.5689 deg

Mean motion: 14.24822429 rev/day

Mean motion (dot): 0.00003346 rev/day2

B* drag term: 0.001334529 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, 10:59 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 33866U 97051AK 25248.95801681 .00003346 00000-0 13345-2 0 9991

TLE line 2: 2 33866 86.3031 134.3818 0113289 113.8510 267.5689 14.24822429854187

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
THOR BURNER 2A R/B SSO 2025-06-03 15:34:18 0.0001103476 338.0 (m) ROCKET BODY
THOR ABLESTAR R/B LEO 2025-01-13 23:27:38 0.0002398801 730.0 (m) ROCKET BODY
NOAA 16 DEB SSO 2024-12-28 03:54:11 0.0001772875 160.0 (m) DEBRIS
CZ-6A DEB LEO 2024-09-18 11:57:20 0.0004970783 223.0 (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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