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 59585U 26145.41967203 +.00000000 +00000-0 +40487-4 0 00002
2 59585 43.0009 296.0049 0002502 274.2628 85.7938 15.27579771 01
| Epoch (UTC): | 25 May 2026 10:04:19 |
| Eccentricity: | 0.0002502 |
| inclination: | 43.0009° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 296.0049° |
| argument of perigee: | 274.2628° |
| revolutions per day: | 15.27579771 |
| mean anomaly at epoch: | 85.7938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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