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 57251U 26145.46181740 +.00000000 +00000-0 +17660-4 0 00006
2 57251 43.0035 306.1159 0001577 267.8999 92.1672 15.27578205 01
| Epoch (UTC): | 25 May 2026 11:05:01 |
| Eccentricity: | 0.0001577 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 306.1159° |
| argument of perigee: | 267.8999° |
| revolutions per day: | 15.27578205 |
| mean anomaly at epoch: | 92.1672° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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