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 59860U 26145.56682995 +.00000000 +00000-0 +64529-4 0 00009
2 59860 43.0007 203.8262 0001745 274.2966 85.7687 15.27580814 02
| Epoch (UTC): | 25 May 2026 13:36:14 |
| Eccentricity: | 0.0001745 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 203.8262° |
| argument of perigee: | 274.2966° |
| revolutions per day: | 15.27580814 |
| mean anomaly at epoch: | 85.7687° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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