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 53402U 26145.37054825 +.00000000 +00000-0 -59002-4 0 00000
2 53402 53.2116 139.8880 0001430 53.4614 306.6510 15.08847652 09
| Epoch (UTC): | 25 May 2026 08:53:35 |
| Eccentricity: | 0.0001430 |
| inclination: | 53.2116° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 139.8880° |
| argument of perigee: | 53.4614° |
| revolutions per day: | 15.08847652 |
| mean anomaly at epoch: | 306.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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