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 59297U 26145.46506275 +.00000000 +00000-0 +52146-4 0 00000
2 59297 43.0003 157.3376 0001213 277.1937 82.8777 15.27579083 05
| Epoch (UTC): | 25 May 2026 11:09:41 |
| Eccentricity: | 0.0001213 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.3376° |
| argument of perigee: | 277.1937° |
| revolutions per day: | 15.27579083 |
| mean anomaly at epoch: | 82.8777° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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