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 57738U 26145.35299716 +.00000000 +00000-0 -59155-4 0 00003
2 57738 43.0011 99.2887 0001326 262.7685 97.3016 15.27588765 02
| Epoch (UTC): | 25 May 2026 08:28:18 |
| Eccentricity: | 0.0001326 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 99.2887° |
| argument of perigee: | 262.7685° |
| revolutions per day: | 15.27588765 |
| mean anomaly at epoch: | 97.3016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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