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

10260

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: 1997-051NY

Object number (NORAD): 35052

Object ID (CCSDS): 35052

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 100.113 minutes

Inclination: 86.3322 deg

SMA: 7141.991 km

Apoapsis: 770.619 km

Periapsis: 757.094 km

RAAN: 44.9514 deg

Eccentricy: 0.00094689

Argument of periapsis: 270.1668 deg

Mean anomaly: 89.8445 deg

Mean motion: 14.38380469 rev/day

Mean motion (dot): 0.00000985 rev/day2

B* drag term: 0.00031692945 1/REarth

Two-line elements (TLE)

Creation date: Oct. 16, 2025, 6:34 p.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Oct. 16, 2025, 2:36 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35052U 97051NY 25289.60833697 .00000985 00000-0 31693-3 0 9992

TLE line 2: 2 35052 86.3322 44.9514 0009469 270.1668 89.8445 14.38380469864547

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
CZ-6A DEB SSO 2025-08-08 01:15:39 0.0001732162 170.0 (m) DEBRIS
CZ-6A DEB SSO 2024-11-09 05:24:07 0.0002156554 906.0 (m) DEBRIS
DELTA 4 DEB SSO 2024-06-03 16:52:12 0.0003211002 523.0 (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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