KAGAYAKI

Satellite information

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Satellite Type and Status

PAYLOADIN ORBIT

Key statistics

Satellite KAGAYAKI at a glance.

Uptime

6169

Days in orbit

Revolutions

≈ 14.7

Per day

Orbit

SSO

Sun Synchronous Orbit

Inclination

98.1

Latest

Satellite identification and parameters

Extended collection of information and parameters for KAGAYAKI.

Object identification

Identified? True

Debris? False

Object name: KAGAYAKI

International designator: 2009-002D

Object number (NORAD): 33495

Object ID (CCSDS): 33495

Country: JAPAN (JPN)

Current information (Y/N): Y

RCS size: MEDIUM

Orbital parameters

Period: 97.654 minutes

Inclination: 98.1349 deg

SMA: 7024.56 km

Apoapsis: 650.883 km

Periapsis: 641.967 km

RAAN: 247.6122 deg

Eccentricy: 0.0006346

Argument of periapsis: 262.8479 deg

Mean anomaly: 97.2008 deg

Mean motion: 14.74599527 rev/day

Mean motion (dot): 0.00000764 rev/day2

B* drag term: 0.00012240983 1/REarth

Two-line elements (TLE)

Creation date: Dec. 14, 2025, 3:07 a.m.

Reference frame: TEME

Reference center: EARTH

Epoch: Dec. 13, 2025, 4:03 p.m. UTC

TLE line 0: 0 KAGAYAKI

TLE line 1: 1 33495U 09002D 25347.66875390 .00000764 00000-0 12241-3 0 9990

TLE line 2: 2 33495 98.1349 247.6122 0006346 262.8479 97.2008 14.74599527906870

Live tracking on map

Real-time ground track for satellite KAGAYAKI.

In-orbit conjunctions

A list of the most updated potential collisions computed for object KAGAYAKI.

Target Orbit TCA Probability of collision Miss distance Type
CZ-6A DEB SSO 2025-05-29 10:02:45 0.0002678041 589.0 (m) DEBRIS
CZ-4 DEB SSO 2024-11-08 15:04:07 0.0001363155 943.0 (m) DEBRIS
THORAD AGENA D DEB LEO 2024-10-25 15:50:09 0.0002597477 492.0 (m) DEBRIS
COSMOS 2251 DEB LEO 2024-07-12 15:36:30 0.0002868578 958.0 (m) DEBRIS
FENGYUN 1C DEB SSO 2024-06-13 15:03:11 0.0001321553 114.0 (m) DEBRIS

Associated space launch

Japanese Earth observation satellite. Launched with 7 secondary payloads.

KAGAYAKI was lifted into orbit during the mission ‘H-IIA 202 | GOSAT’, on board a H-IIA space rocket.

The launch took place on Jan. 23, 2009, 3:54 a.m. from Yoshinobu Launch Complex LP-1.

For more information about the launch, click the button.

Launch to space H-IIA 202 | GOSAT
H-IIA 202 | GOSAT

Agency: N/A

Status: Launch Successful

Launch date: Jan. 23, 2009, 3:54 a.m. UTC

Rocket: H-IIA

Launch pad: Yoshinobu Launch Complex LP-1

Location: Tanegashima Space Center, Japan

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