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

≈ 14.4

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: 1997-051PP

Object number (NORAD): 35299

Object ID (CCSDS): 35299

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 99.998 minutes

Inclination: 86.2859 deg

SMA: 7136.529 km

Apoapsis: 800.175 km

Periapsis: 716.612 km

RAAN: 78.5085 deg

Eccentricy: 0.0058546

Argument of periapsis: 85.4017 deg

Mean anomaly: 330.9425 deg

Mean motion: 14.40032245 rev/day

Mean motion (dot): 0.00003666 rev/day2

B* drag term: 0.0011343239 1/REarth

Two-line elements (TLE)

Creation date: Aug. 31, 2025, 2:26 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Aug. 30, 2025, 1:26 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35299U 97051PP 25242.56034209 .00003666 00000-0 11343-2 0 9999

TLE line 2: 2 35299 86.2859 78.5085 0058546 85.4017 330.9425 14.40032245848319

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
SL-8 R/B LEO 2025-08-01 19:03:26 0.0001030757 656.0 (m) ROCKET BODY
PEGASUS DEB LEO 2025-06-28 07:55:10 0.0001127152 656.0 (m) DEBRIS
CZ-2C R/B SSO 2025-06-26 20:03:11 0.0005685328 263.0 (m) ROCKET BODY
CZ-6A DEB LEO 2025-04-17 21:59:14 0.001476617 45.0 (m) DEBRIS
ADEOS SSO 2024-12-04 04:44:17 0.0009017441 134.0 (m) PAYLOAD

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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