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 59246U 26145.49256543 +.00000000 +00000-0 +61786-4 0 00007
2 59246 43.0001 69.6590 0001257 274.2495 85.8213 15.27573278 03
| Epoch (UTC): | 25 May 2026 11:49:17 |
| Eccentricity: | 0.0001257 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 69.6590° |
| argument of perigee: | 274.2495° |
| revolutions per day: | 15.27573278 |
| mean anomaly at epoch: | 85.8213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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