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Hodoyoshi 4

In orbit NORAD 40011 XPNP-4397-0346-9738-4793 Japan

2014

Launch

0

Observations all time

Mission information
Spacecraft name
Hodoyoshi 4
Other names
2014-033B, "Reasonably Reliable Systems"
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
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
584.74 km
Apogee
615.44 km
Inclination
97.5°
Period
96.8 min
Semi-major axis
6978.2 km
Velocity
7.55 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:36 UTC
Two-line elements (TLE)
1 40011U 14033B   26283.94679498  .00001207  00000-0  13553-3 0  9994
2 40011 97.5474 103.2378 0021996 283.2166 76.6598 14.88354427666020
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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 14:45:52 HODOYOSHI-4
NORAD 40011
CZ-2D R/B
NORAD 65853
2.058 13.50 5.6e-07
2026-10-11 22:05:44 HODOYOSHI-4
NORAD 40011
COSMOS 2251 DEB
NORAD 35764
2.751 3.09 5.7e-07
2026-10-12 09:49:52 HODOYOSHI-4
NORAD 40011
PEGASUS DEB
NORAD 27679
3.259 15.12 1.4e-07
2026-10-13 03:32:14 HODOYOSHI-4
NORAD 40011
GRITSS
NORAD 69931
3.105 9.59 3.7e-07
2026-10-13 07:55:52 HODOYOSHI-4
NORAD 40011
THORAD AGENA D DEB
NORAD 4311
4.956 3.71 1.7e-07
2026-10-14 11:48:27 HODOYOSHI-4
NORAD 40011
ET-001C
NORAD 69942
3.299 9.59 3.2e-07
2026-10-14 15:02:11 HODOYOSHI-4
NORAD 40011
NULINK-2
NORAD 68994
2.706 9.24 4.9e-07
2026-10-14 19:08:35 HODOYOSHI-4
NORAD 40011
PRISMA
NORAD 44072
1.502 11.95 1.3e-06
2026-10-15 16:47:40 HODOYOSHI-4
NORAD 40011
AE1A
NORAD 68487
1.404 13.96 1.1e-06
2026-10-15 20:01:16 HODOYOSHI-4
NORAD 40011
ICEYE-X73
NORAD 68496
2.877 13.96 2.6e-07
2026-10-16 01:46:40 HODOYOSHI-4
NORAD 40011
UNKNOWN
NORAD 81371
2.797 6.58 5.1e-07
2026-10-16 02:28:40 HODOYOSHI-4
NORAD 40011
SL-24 R/B
NORAD 31699
3.651 14.02 1.6e-07
2026-10-16 17:09:26 HODOYOSHI-4
NORAD 40011
CZ-4B DEB
NORAD 39052
4.687 13.49 1.1e-07
2026-10-16 18:52:37 HODOYOSHI-4
NORAD 40011
CZ-4C DEB
NORAD 39212
1.251 14.79 1.1e-06
2026-10-17 06:26:14 HODOYOSHI-4
NORAD 40011
CAPELLA-18 (ACADIA-8)
NORAD 67385
1.832 14.97 4.7e-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