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

10096

Days in orbit

Revolutions

≈ 14.5

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: 1997-051VM

Object number (NORAD): 36080

Object ID (CCSDS): 36080

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.63 minutes

Inclination: 86.3159 deg

SMA: 7119.009 km

Apoapsis: 752.734 km

Periapsis: 729.014 km

RAAN: 106.5624 deg

Eccentricy: 0.001666

Argument of periapsis: 188.0314 deg

Mean anomaly: 172.0624 deg

Mean motion: 14.45351403 rev/day

Mean motion (dot): 0.00003844 rev/day2

B* drag term: 0.0010869 1/REarth

Two-line elements (TLE)

Creation date: May 2, 2025, 2:33 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: April 30, 2025, 5:30 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 36080U 97051VM 25120.22929943 .00003844 00000-0 10869-2 0 9994

TLE line 2: 2 36080 86.3159 106.5624 0016660 188.0314 172.0624 14.45351403441415

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 2025-01-13 08:48:04 0.0004239396 68.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-09-28 05:16:57 0.0003442063 797.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-09-27 09:28:38 0.000123018 836.0 (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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