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 59393U 26145.26996528 +.00000000 +00000-0 +44307-4 0 00009
2 59393 53.1618 246.4662 0001065 76.3435 283.7686 15.34388225 06
| Epoch (UTC): | 25 May 2026 06:28:45 |
| Eccentricity: | 0.0001065 |
| inclination: | 53.1618° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 246.4662° |
| argument of perigee: | 76.3435° |
| revolutions per day: | 15.34388225 |
| mean anomaly at epoch: | 283.7686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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