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

10103

Days in orbit

Revolutions

≈ 14.8

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.2

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: 1997-051QU

Object number (NORAD): 35622

Object ID (CCSDS): 35622

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 97.006 minutes

Inclination: 86.2132 deg

SMA: 6993.469 km

Apoapsis: 624.809 km

Periapsis: 605.86 km

RAAN: 7.1039 deg

Eccentricy: 0.0013548

Argument of periapsis: 340.1125 deg

Mean anomaly: 37.4275 deg

Mean motion: 14.84443785 rev/day

Mean motion (dot): 0.00016125 rev/day2

B* drag term: 0.0019084 1/REarth

Two-line elements (TLE)

Creation date: May 12, 2025, 2:31 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 11, 2025, 10:01 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35622U 97051QU 25131.91768744 .00016125 00000-0 19084-2 0 9997

TLE line 2: 2 35622 86.2132 7.1039 0013548 340.1125 37.4275 14.84443785841581

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
PSLV R/B SSO 2025-02-19 08:23:58 0.001491069 79.0 (m) ROCKET BODY
SL-14 R/B LEO 2024-12-07 10:40:58 0.0001004622 660.0 (m) ROCKET BODY
CZ-6A DEB LEO 2024-10-07 10:31:40 0.000353396 684.0 (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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