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

10213

Days in orbit

Revolutions

≈ 14.2

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.1

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: 1997-051RJ

Object number (NORAD): 35680

Object ID (CCSDS): 35680

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 101.5 minutes

Inclination: 86.0991 deg

SMA: 7207.844 km

Apoapsis: 943.657 km

Periapsis: 715.76 km

RAAN: 67.9015 deg

Eccentricy: 0.01580895

Argument of periapsis: 252.3174 deg

Mean anomaly: 121.5895 deg

Mean motion: 14.18713607 rev/day

Mean motion (dot): 0.00004817 rev/day2

B* drag term: 0.0020432739 1/REarth

Two-line elements (TLE)

Creation date: Aug. 30, 2025, 3:38 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 29, 2025, 7:14 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35680U 97051RJ 25241.80167277 .00004817 00000-0 20433-2 0 9990

TLE line 2: 2 35680 86.0991 67.9015 0158089 252.3174 121.5895 14.18713607592128

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 2025-08-26 00:36:20 0.0001424411 145.0 (m) DEBRIS
METEOR 2-17 DEB LEO 2024-09-27 10:48:34 0.0001801157 760.0 (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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