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 53397U 26145.40366632 +.00000000 +00000-0 +23557-4 0 00004
2 53397 53.2141 139.7349 0001235 98.1786 261.9346 15.08839684 04
| Epoch (UTC): | 25 May 2026 09:41:16 |
| Eccentricity: | 0.0001235 |
| inclination: | 53.2141° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 139.7349° |
| argument of perigee: | 98.1786° |
| revolutions per day: | 15.08839684 |
| mean anomaly at epoch: | 261.9346° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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