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

≈ 14.8

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: 1997-051CX

Object number (NORAD): 34088

Object ID (CCSDS): 34088

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 97.281 minutes

Inclination: 86.3859 deg

SMA: 7006.665 km

Apoapsis: 629.762 km

Periapsis: 627.298 km

RAAN: 130.7857 deg

Eccentricy: 0.0001758

Argument of periapsis: 270.4986 deg

Mean anomaly: 212.7133 deg

Mean motion: 14.80252199 rev/day

Mean motion (dot): 0.00018763 rev/day2

B* drag term: 0.002459 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, 1:26 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34088U 97051CX 25126.56031497 .00018763 00000-0 24590-2 0 9993

TLE line 2: 2 34088 86.3859 130.7857 0001758 270.4986 212.7133 14.80252199854751

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
MAST SSO 2025-01-12 03:14:14 0.000300596 574.0 (m) PAYLOAD
FENGYUN 1C DEB SSO 2024-11-27 17:01:59 0.0002259919 51.0 (m) DEBRIS
CZ-4C R/B LEO 2024-11-21 19:09:02 0.0006002316 349.0 (m) ROCKET BODY
SINAH 1 SSO 2024-09-25 06:47:54 0.0001213065 804.0 (m) PAYLOAD
CZ-6A DEB SSO 2024-06-09 17:23:08 0.0001908505 369.0 (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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