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 57820U 26145.34400002 +.00000000 +00000-0 -22104-4 0 00000
2 57820 43.0027 161.0845 0001354 276.6874 83.3824 15.27566231 04
| Epoch (UTC): | 25 May 2026 08:15:21 |
| Eccentricity: | 0.0001354 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 161.0845° |
| argument of perigee: | 276.6874° |
| revolutions per day: | 15.27566231 |
| mean anomaly at epoch: | 83.3824° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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