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 53807U 26070.16630697 +.00000000 +00000-0 +20297-3 0 00002
2 53807 53.2291 133.7521 0004743 229.6889 130.3702 15.37172731 04
| Epoch (UTC): | 11 March 2026 03:59:28 |
| Eccentricity: | 0.0004743 |
| inclination: | 53.2291° |
| perigee height: | 451 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 133.7521° |
| argument of perigee: | 229.6889° |
| revolutions per day: | 15.37172731 |
| mean anomaly at epoch: | 130.3702° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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