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 57130U 26145.43727571 +.00000000 +00000-0 +22080-4 0 00009
2 57130 43.0037 207.8055 0001689 266.2949 93.7710 15.26740190 06
| Epoch (UTC): | 25 May 2026 10:29:40 |
| Eccentricity: | 0.0001689 |
| inclination: | 43.0037° |
| perigee height: | 484 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 207.8055° |
| argument of perigee: | 266.2949° |
| revolutions per day: | 15.26740190 |
| mean anomaly at epoch: | 93.7710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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