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 59702U 26145.58761103 +.00000000 +00000-0 -12997-3 0 00007
2 59702 43.0031 345.5363 0000742 265.7853 94.2914 15.27584238 08
| Epoch (UTC): | 25 May 2026 14:06:09 |
| Eccentricity: | 0.0000742 |
| inclination: | 43.0031° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.5363° |
| argument of perigee: | 265.7853° |
| revolutions per day: | 15.27584238 |
| mean anomaly at epoch: | 94.2914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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