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 59310U 26145.33605925 +.00000000 +00000-0 +44694-4 0 00003
2 59310 43.0018 154.6324 0001068 277.2969 82.7761 15.27578882 02
| Epoch (UTC): | 25 May 2026 08:03:55 |
| Eccentricity: | 0.0001068 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 154.6324° |
| argument of perigee: | 277.2969° |
| revolutions per day: | 15.27578882 |
| mean anomaly at epoch: | 82.7761° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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