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 65363U 26145.58335647 +.00000000 +00000-0 +11293-2 0 00003
2 65363 53.1591 171.0635 0000946 70.3996 62.4470 15.33531966 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0000946 |
| inclination: | 53.1591° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 171.0635° |
| argument of perigee: | 70.3996° |
| revolutions per day: | 15.33531966 |
| mean anomaly at epoch: | 62.4470° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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