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 57026U 26145.59956318 +.00000000 +00000-0 +46096-3 0 00005
2 57026 97.4936 258.5851 0006678 137.6219 222.5541 15.34889207 08
| Epoch (UTC): | 25 May 2026 14:23:22 |
| Eccentricity: | 0.0006678 |
| inclination: | 97.4936° |
| perigee height: | 457 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 258.5851° |
| argument of perigee: | 137.6219° |
| revolutions per day: | 15.34889207 |
| mean anomaly at epoch: | 222.5541° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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