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

10098

Days in orbit

Revolutions

≈ 14.4

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: 1997-051ABR

Object number (NORAD): 46734

Object ID (CCSDS): 46734

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.978 minutes

Inclination: 86.2611 deg

SMA: 7135.597 km

Apoapsis: 786.21 km

Periapsis: 728.713 km

RAAN: 99.5315 deg

Eccentricy: 0.0040289

Argument of periapsis: 342.5964 deg

Mean anomaly: 79.848 deg

Mean motion: 14.40314467 rev/day

Mean motion (dot): 0.00004733 rev/day2

B* drag term: 0.0014737 1/REarth

Two-line elements (TLE)

Creation date: May 7, 2025, 3:14 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 6, 2025, 5:26 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 46734U 97051ABR 25126.22639068 .00004733 00000-0 14737-2 0 9999

TLE line 2: 2 46734 86.2611 99.5315 0040289 342.5964 79.8480 14.40314467598358

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 2056 LEO 2025-03-21 04:54:23 0.0003702611 201.0 (m) PAYLOAD
CZ-6A DEB SSO 2024-11-13 05:08:05 0.0004620062 166.0 (m) DEBRIS
SL-14 DEB LEO 2024-11-12 06:21:22 0.0001910355 975.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-09-27 02:57:45 0.0002030952 314.0 (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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