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 59300U 26145.49704880 +.00000000 +00000-0 +32392-3 0 00000
2 59300 43.0010 156.7174 0001498 290.4789 69.5902 15.27603537 09
| Epoch (UTC): | 25 May 2026 11:55:45 |
| Eccentricity: | 0.0001498 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 156.7174° |
| argument of perigee: | 290.4789° |
| revolutions per day: | 15.27603537 |
| mean anomaly at epoch: | 69.5902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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