Key statistics
Satellite KAGAYAKI at a glance.
Uptime
6113
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: 97.66 minutes
Inclination: 98.1344 deg
SMA: 7024.887 km
Apoapsis: 653.145 km
Periapsis: 640.36 km
RAAN: 191.6665 deg
Eccentricy: 0.00090995
Argument of periapsis: 82.4479 deg
Mean anomaly: 277.7763 deg
Mean motion: 14.74496369 rev/day
Mean motion (dot): 0.00000898 rev/day2
B* drag term: 0.00014278855 1/REarth
Two-line elements (TLE)
Creation date: Oct. 19, 2025, 2:20 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Oct. 18, 2025, 10:58 p.m. UTC
TLE line 0: 0 KAGAYAKI
TLE line 1: 1 33495U 09002D 25291.95715947 .00000898 00000-0 14279-3 0 9992
TLE line 2: 2 33495 98.1344 191.6665 0009100 82.4479 277.7763 14.74496369898662
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.
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.

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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