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 59874U 26145.43221178 +.00000000 +00000-0 +11644-3 0 00001
2 59874 43.0018 204.5372 0001835 279.2080 80.8564 15.27576231 09
| Epoch (UTC): | 25 May 2026 10:22:23 |
| Eccentricity: | 0.0001835 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5372° |
| argument of perigee: | 279.2080° |
| revolutions per day: | 15.27576231 |
| mean anomaly at epoch: | 80.8564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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