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

10261

Days in orbit

Revolutions

≈ 14.5

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: 1997-051NF

Object number (NORAD): 34926

Object ID (CCSDS): 34926

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.226 minutes

Inclination: 86.133 deg

SMA: 7099.763 km

Apoapsis: 783.532 km

Periapsis: 659.724 km

RAAN: 34.8157 deg

Eccentricy: 0.00871917

Argument of periapsis: 127.3701 deg

Mean anomaly: 288.5116 deg

Mean motion: 14.51232454 rev/day

Mean motion (dot): 0.00023336 rev/day2

B* drag term: 0.0055718414 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, 7:51 a.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 34926U 97051NF 25289.32739822 .00023336 00000-0 55718-2 0 9993

TLE line 2: 2 34926 86.1330 34.8157 0087192 127.3701 288.5116 14.51232454856239

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
COSMOS 1275 DEB LEO 2025-03-18 02:48:14 0.0001086257 224.0 (m) DEBRIS
IRIDIUM 920 LEO 2025-02-25 20:35:40 0.0001554715 147.0 (m) PAYLOAD
CZ-6A DEB LEO 2025-02-09 17:06:06 0.0003934275 434.0 (m) DEBRIS
CZ-6A DEB SSO 2024-12-26 03:28:35 0.0002274857 49.0 (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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