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 53396U 26145.26014808 +.00000000 +00000-0 +40945-4 0 00002
2 53396 53.2138 140.3831 0000999 73.2360 286.8741 15.08840424 00
| Epoch (UTC): | 25 May 2026 06:14:36 |
| Eccentricity: | 0.0000999 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 140.3831° |
| argument of perigee: | 73.2360° |
| revolutions per day: | 15.08840424 |
| mean anomaly at epoch: | 286.8741° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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