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

≈ 14.5

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: 1997-051ACE

Object number (NORAD): 46972

Object ID (CCSDS): 46972

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.341 minutes

Inclination: 86.3879 deg

SMA: 7105.239 km

Apoapsis: 735.305 km

Periapsis: 718.903 km

RAAN: 134.2217 deg

Eccentricy: 0.0011542

Argument of periapsis: 117.5764 deg

Mean anomaly: 257.7576 deg

Mean motion: 14.49554997 rev/day

Mean motion (dot): 0.00002724 rev/day2

B* drag term: 0.00070453 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, 6:40 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 46972U 97051ACE 25126.27822774 .00002724 00000-0 70453-3 0 9992

TLE line 2: 2 46972 86.3879 134.2217 0011542 117.5764 257.7576 14.49554997583782

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
CHUANG XIN 1 (CZ-1) SSO 2025-04-18 04:58:53 0.0005659935 160.0 (m) PAYLOAD

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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