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

10158

Days in orbit

Revolutions

≈ 14.5

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: 1997-051KM

Object number (NORAD): 34690

Object ID (CCSDS): 34690

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.025 minutes

Inclination: 86.3774 deg

SMA: 7090.167 km

Apoapsis: 718.42 km

Periapsis: 705.644 km

RAAN: 106.272 deg

Eccentricy: 0.0009009

Argument of periapsis: 171.7925 deg

Mean anomaly: 344.2994 deg

Mean motion: 14.54179662 rev/day

Mean motion (dot): 0.00001577 rev/day2

B* drag term: 0.00036784 1/REarth

Two-line elements (TLE)

Creation date: July 6, 2025, 6:05 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 6, 2025, 6:21 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34690U 97051KM 25187.26508360 .00001577 00000-0 36784-3 0 9998

TLE line 2: 2 34690 86.3774 106.2720 0009009 171.7925 344.2994 14.54179662857760

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-4 DEB SSO 2024-11-14 10:04:19 0.0001887771 50.0 (m) DEBRIS
NOAA 16 DEB SSO 2024-07-21 15:57:28 0.0008996615 46.0 (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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