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HODOYOSHI 3

In orbit NORAD 40015 CODJ-5300-8734-2552-4197 Japan

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2014

Launch

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Observations all time

Mission information
Spacecraft name
HODOYOSHI 3
Other names
2014-033F
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2014-06-19 00:00:00
Separation time
2014-06-19 00:00:00
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
586.30 km
Apogee
631.19 km
Inclination
97.7°
Period
96.9 min
Semi-major axis
6986.9 km
Velocity
7.53 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:17 UTC
Two-line elements (TLE)
1 40015U 14033F   26282.89759292  .00000787  00000-0  96316-4 0  9993
2 40015  97.6556  81.4394 0032118 339.1242  20.8660 14.85593797664655
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-11 00:20:57 HODOYOSHI-3
NORAD 40015 		CZ-6A DEB
NORAD 60634 		4.365 15.02 7.9e-08
2026-10-11 04:28:52 HODOYOSHI-3
NORAD 40015 		DELTA 1 DEB
NORAD 7892 		1.068 14.77 1.5e-06
2026-10-12 15:59:39 HODOYOSHI-3
NORAD 40015 		CZ-6A DEB
NORAD 61453 		4.989 15.11 6.0e-08
2026-10-12 18:16:19 HODOYOSHI-3
NORAD 40015 		KUIPER-00081
NORAD 65132 		4.041 14.54 1.1e-07
2026-10-13 01:10:06 HODOYOSHI-3
NORAD 40015 		CZ-6A DEB
NORAD 56273 		4.559 12.36 1.4e-07
2026-10-13 05:55:25 HODOYOSHI-3
NORAD 40015 		FIRESAT3
NORAD 69890 		1.515 11.49 1.3e-06
2026-10-13 11:38:48 HODOYOSHI-3
NORAD 40015 		FENGYUN 1C DEB
NORAD 35147 		3.118 3.39 4.4e-07
2026-10-13 22:58:05 HODOYOSHI-3
NORAD 40015 		PLEIADES NEO 4
NORAD 49070 		3.985 10.13 2.2e-07
2026-10-14 03:06:30 HODOYOSHI-3
NORAD 40015 		RCM-3
NORAD 44323 		0.838 14.55 2.6e-06
2026-10-14 14:36:11 HODOYOSHI-3
NORAD 40015 		CZ-2D R/B
NORAD 65853 		4.571 13.51 1.1e-07
2026-10-14 15:57:22 HODOYOSHI-3
NORAD 40015 		CZ-6A DEB
NORAD 56271 		1.904 11.53 8.5e-07
2026-10-15 01:01:21 HODOYOSHI-3
NORAD 40015 		FENGYUN 1C DEB
NORAD 30755 		4.022 14.88 1.0e-07
2026-10-15 06:27:47 HODOYOSHI-3
NORAD 40015 		SL-14 R/B
NORAD 11267 		2.547 14.90 5.9e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite