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

≈ 14.6

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: 1997-051ABX

Object number (NORAD): 46965

Object ID (CCSDS): 46965

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.707 minutes

Inclination: 86.334 deg

SMA: 7074.992 km

Apoapsis: 711.278 km

Periapsis: 682.437 km

RAAN: 53.019 deg

Eccentricy: 0.0020382

Argument of periapsis: 153.7048 deg

Mean anomaly: 23.3687 deg

Mean motion: 14.58860581 rev/day

Mean motion (dot): 0.00001858 rev/day2

B* drag term: 0.00039145 1/REarth

Two-line elements (TLE)

Creation date: July 2, 2025, 5:47 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: July 2, 2025, 9:14 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 46965U 97051ABX 25183.38486572 .00001858 00000-0 39145-3 0 9991

TLE line 2: 2 46965 86.3340 53.0190 0020382 153.7048 23.3687 14.58860581598857

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
MOZ.5/SAFIR/RUBIN 5/SL-8 SSO 2025-05-16 11:39:36 0.0001446681 509.0 (m) PAYLOAD
ATLAS F BURNER 2 R/B SSO 2024-09-26 15:32:49 0.0003627339 769.0 (m) ROCKET BODY

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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