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 59515U 26145.55283115 +.00000000 +00000-0 -10270-3 0 00000
2 59515 43.0015 243.6989 0001187 263.9848 96.0869 15.27597563 06
| Epoch (UTC): | 25 May 2026 13:16:04 |
| Eccentricity: | 0.0001187 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.6989° |
| argument of perigee: | 263.9848° |
| revolutions per day: | 15.27597563 |
| mean anomaly at epoch: | 96.0869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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