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 59412U 26145.58169282 +.00000000 +00000-0 +11945-3 0 00006
2 59412 43.0023 342.0726 0002262 284.1244 75.9356 15.27584751 06
| Epoch (UTC): | 25 May 2026 13:57:38 |
| Eccentricity: | 0.0002262 |
| inclination: | 43.0023° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 342.0726° |
| argument of perigee: | 284.1244° |
| revolutions per day: | 15.27584751 |
| mean anomaly at epoch: | 75.9356° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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