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 53059U 26145.43164277 +.00000000 +00000-0 -50360-4 0 00006
2 53059 97.4484 325.3396 0001163 100.8696 259.2663 15.05655453 04
| Epoch (UTC): | 25 May 2026 10:21:33 |
| Eccentricity: | 0.0001163 |
| inclination: | 97.4484° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 325.3396° |
| argument of perigee: | 100.8696° |
| revolutions per day: | 15.05655453 |
| mean anomaly at epoch: | 259.2663° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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