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

10096

Days in orbit

Revolutions

≈ 14.6

Per day

Orbit

LEO

Low Earth Orbit

Inclination

86.2

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: 1997-051PF

Object number (NORAD): 35080

Object ID (CCSDS): 35080

Country: UNITED STATES OF AMERICA (US)

Current information (Y/N): Y

RCS size: SMALL

Orbital parameters

Period: 98.415 minutes

Inclination: 86.217 deg

SMA: 7061.025 km

Apoapsis: 742.642 km

Periapsis: 623.138 km

RAAN: 155.6789 deg

Eccentricy: 0.0084622

Argument of periapsis: 219.9968 deg

Mean anomaly: 139.4993 deg

Mean motion: 14.63191464 rev/day

Mean motion (dot): 0.00034887 rev/day2

B* drag term: 0.0064086 1/REarth

Two-line elements (TLE)

Creation date: May 6, 2025, 3:54 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: May 5, 2025, 12:19 p.m. UTC

TLE line 0: 0 IRIDIUM 33 DEB

TLE line 1: 1 35080U 97051PF 25125.51350387 .00034887 00000-0 64086-2 0 9991

TLE line 2: 2 35080 86.2170 155.6789 0084622 219.9968 139.4993 14.63191464664349

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
NOAA 12 SSO 2025-01-24 06:15:10 0.0001314395 1000.0 (m) PAYLOAD
CZ-6A DEB LEO 2024-10-23 14:37:17 0.0002518831 144.0 (m) DEBRIS
THOR BURNER 2 R/B SSO 2024-10-02 02:25:57 0.000793791 199.0 (m) ROCKET BODY

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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