View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53400U 26145.37422837 +.00000000 +00000-0 +95944-4 0 00004
2 53400 53.2112 139.8706 0001023 71.6249 288.4854 15.08838110 01
| Epoch (UTC): | 25 May 2026 08:58:53 |
| Eccentricity: | 0.0001023 |
| inclination: | 53.2112° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 139.8706° |
| argument of perigee: | 71.6249° |
| revolutions per day: | 15.08838110 |
| mean anomaly at epoch: | 288.4854° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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