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PROITERES

In orbit NORAD 38756 NHVG-4421-1523-2154-0492 Japan

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Launch

1

Observations all time

Mission information
Spacecraft name
PROITERES
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
609.60 km
Apogee
626.29 km
Inclination
98.2°
Period
97.1 min
Semi-major axis
6996.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:44 UTC
Two-line elements (TLE)
1 38756U 12047B   26280.90398096  .00001256  00000-0  16272-3 0  9990
2 38756 98.2342 205.9798 0011930 53.7374 306.4939 14.82674940759013
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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 14:11:14 GEESAT-1 07
NORAD 52791
PROITERES
NORAD 38756
4.613 14.45 8.9e-08
2026-10-12 14:21:02 KUIPER-00261
NORAD 67158
PROITERES
NORAD 38756
3.916 6.33 2.6e-07
2026-10-13 00:06:35 KUIPER-00076
NORAD 64823
PROITERES
NORAD 38756
3.463 14.36 1.6e-07
2026-10-13 08:22:42 THEOS-2 (T2V)
NORAD 58016
PROITERES
NORAD 38756
3.618 14.18 1.6e-07
2026-10-13 14:47:37 KUIPER-00644
NORAD 69788
PROITERES
NORAD 38756
4.949 11.61 1.2e-07
2026-10-14 15:52:12 SHERPA-LTC2
NORAD 53754
PROITERES
NORAD 38756
2.805 13.88 2.8e-07
2026-10-15 21:51:42 KUIPER-00616
NORAD 69775
PROITERES
NORAD 38756
1.148 12.24 2.2e-06
2026-10-16 03:56:44 KUIPER-00081
NORAD 65132
PROITERES
NORAD 38756
3.745 7.39 2.8e-07
2026-10-16 09:01:52 KUIPER-00079
NORAD 64826
PROITERES
NORAD 38756
2.128 14.52 4.1e-07
2026-10-16 18:55:05 KUIPER-00526
NORAD 69764
PROITERES
NORAD 38756
1.517 11.59 1.3e-06
2026-10-16 20:28:09 KUIPER-00448
NORAD 68871
PROITERES
NORAD 38756
1.421 14.15 1.0e-06
2026-10-17 02:36:18 GEESAT-4 09
NORAD 65127
PROITERES
NORAD 38756
4.510 13.98 1.1e-07
2026-10-17 05:56:07 KUIPER-00091
NORAD 64836
PROITERES
NORAD 38756
2.861 14.51 2.3e-07
2026-10-17 12:40:06 KUIPER-00547
NORAD 69615
PROITERES
NORAD 38756
4.532 7.71 1.9e-07
2026-10-17 18:44:27 KUIPER-00180
NORAD 67768
PROITERES
NORAD 38756
3.950 11.12 2.0e-07
2026-10-18 01:41:11 KUIPER-00639
NORAD 69786
PROITERES
NORAD 38756
2.466 12.77 4.4e-07
2026-10-18 04:50:38 KUIPER-00364
NORAD 68867
PROITERES
NORAD 38756
1.853 14.27 5.8e-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