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 59516U 26145.32724220 +.00000000 +00000-0 +36141-3 0 00007
2 59516 43.0017 245.4428 0001732 278.1548 81.9107 15.27618722 07
| Epoch (UTC): | 25 May 2026 07:51:13 |
| Eccentricity: | 0.0001732 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 245.4428° |
| argument of perigee: | 278.1548° |
| revolutions per day: | 15.27618722 |
| mean anomaly at epoch: | 81.9107° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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