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 57101U 26145.46637718 +.00000000 +00000-0 +30972-4 0 00002
2 57101 43.0029 208.0264 0001160 267.7636 92.3082 15.27577674 06
| Epoch (UTC): | 25 May 2026 11:11:34 |
| Eccentricity: | 0.0001160 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.0264° |
| argument of perigee: | 267.7636° |
| revolutions per day: | 15.27577674 |
| mean anomaly at epoch: | 92.3082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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