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

10268

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: 1997-051MH

Object number (NORAD): 34833

Object ID (CCSDS): 34833

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.184 minutes

Inclination: 86.3915 deg

SMA: 7097.749 km

Apoapsis: 732.545 km

Periapsis: 706.682 km

RAAN: 72.0543 deg

Eccentricy: 0.00182192

Argument of periapsis: 260.1566 deg

Mean anomaly: 252.023 deg

Mean motion: 14.5185023 rev/day

Mean motion (dot): 0.00005145 rev/day2

B* drag term: 0.0012704801 1/REarth

Two-line elements (TLE)

Creation date: Oct. 25, 2025, 3:11 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 24, 2025, 8:16 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34833U 97051MH 25297.84466980 .00005145 00000-0 12705-2 0 9995

TLE line 2: 2 34833 86.3915 72.0543 0018219 260.1566 252.0230 14.51850230870056

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
AEROCUBE 2 SSO 2025-02-13 08:27:50 0.0002712885 126.0 (m) PAYLOAD
NOAA 16 DEB SSO 2024-09-27 04:47:24 0.0001369952 670.0 (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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