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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
615.45 km
Inclination
97.5°
Period
96.8 min
Semi-major axis
6978.2 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-12 05:08:33 UTC
Two-line elements (TLE)
1 40011U 14033B   26284.95524316  .00001104  00000-0  12441-3 0  9995
2 40011 97.5471 104.1986 0022028 279.7494 80.1236 14.88356092666178
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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
2026-10-12 09:49:52 HODOYOSHI-4
NORAD 40011
PEGASUS DEB
NORAD 27679
3.198 15.12 1.5e-07
2026-10-13 03:32:14 HODOYOSHI-4
NORAD 40011
GRITSS
NORAD 69931
2.603 9.59 5.2e-07
2026-10-13 04:16:26 HODOYOSHI-4
NORAD 40011
SL-16 DEB
NORAD 39886
4.149 9.21 2.1e-07
2026-10-14 04:48:21 HODOYOSHI-4
NORAD 40011
GEESAT-3 07
NORAD 61017
3.520 13.93 1.8e-07
2026-10-14 15:30:33 HODOYOSHI-4
NORAD 40011
AETHER-10
NORAD 67381
4.900 14.97 6.6e-08
2026-10-14 19:08:35 HODOYOSHI-4
NORAD 40011
PRISMA
NORAD 44072
2.165 11.95 6.3e-07
2026-10-15 16:47:40 HODOYOSHI-4
NORAD 40011
AE1A
NORAD 68487
1.976 13.96 5.6e-07
2026-10-15 20:54:40 HODOYOSHI-4
NORAD 40011
IRIDIUM 33 DEB
NORAD 33884
3.216 13.22 2.4e-07
2026-10-16 01:46:40 HODOYOSHI-4
NORAD 40011
UNKNOWN
NORAD 81371
2.972 6.58 4.6e-07
2026-10-16 02:28:40 HODOYOSHI-4
NORAD 40011
SL-24 R/B
NORAD 31699
3.828 14.02 1.5e-07
2026-10-16 21:58:05 HODOYOSHI-4
NORAD 40011
LEAP-1
NORAD 65321
4.645 12.03 1.4e-07
2026-10-17 06:26:11 HODOYOSHI-4
NORAD 40011
CAPELLA-18 (ACADIA-8)
NORAD 67385
2.269 14.97 3.1e-07
2026-10-17 08:03:03 HODOYOSHI-4
NORAD 40011
CAPELLA-18 (ACADIA-8)
NORAD 67385
4.748 14.97 7.0e-08
2026-10-17 12:27:29 HODOYOSHI-4
NORAD 40011
PAKTES 1A
NORAD 43529
3.881 2.23 2.9e-07
2026-10-17 18:26:17 HODOYOSHI-4
NORAD 40011
GEESAT-4 04
NORAD 65122
2.690 14.48 2.6e-07
2026-10-17 20:29:03 HODOYOSHI-4
NORAD 40011
FOREST-18 (MANGOSHRIKHAND)
NORAD 68999
4.084 9.24 2.2e-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