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 59318U 26145.50089670 +.00000000 +00000-0 -43294-4 0 00009
2 59318 43.0017 156.7431 0001735 286.7350 73.3311 15.27578187 06
| Epoch (UTC): | 25 May 2026 12:01:17 |
| Eccentricity: | 0.0001735 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 156.7431° |
| argument of perigee: | 286.7350° |
| revolutions per day: | 15.27578187 |
| mean anomaly at epoch: | 73.3311° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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