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 59315U 26145.49320669 +.00000000 +00000-0 +25359-4 0 00001
2 59315 43.0032 156.6903 0001441 295.6525 64.4178 15.27568460 05
| Epoch (UTC): | 25 May 2026 11:50:13 |
| Eccentricity: | 0.0001441 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 156.6903° |
| argument of perigee: | 295.6525° |
| revolutions per day: | 15.27568460 |
| mean anomaly at epoch: | 64.4178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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