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 59416U 26145.55727325 +.00000000 +00000-0 +20778-4 0 00000
2 59416 43.0016 341.8897 0001089 266.6213 93.4514 15.27577759 06
| Epoch (UTC): | 25 May 2026 13:22:28 |
| Eccentricity: | 0.0001089 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 341.8897° |
| argument of perigee: | 266.6213° |
| revolutions per day: | 15.27577759 |
| mean anomaly at epoch: | 93.4514° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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