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 59500U 26145.27304604 +.00000000 +00000-0 -23184-4 0 00009
2 59500 43.0005 227.0926 0001006 254.9774 105.0966 15.27579496 08
| Epoch (UTC): | 25 May 2026 06:33:11 |
| Eccentricity: | 0.0001006 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 227.0926° |
| argument of perigee: | 254.9774° |
| revolutions per day: | 15.27579496 |
| mean anomaly at epoch: | 105.0966° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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