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 57699U 26145.38293708 +.00000000 +00000-0 -66706-4 0 00007
2 57699 43.0042 33.5464 0001159 269.5839 90.4880 15.27571224 09
| Epoch (UTC): | 25 May 2026 09:11:25 |
| Eccentricity: | 0.0001159 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5464° |
| argument of perigee: | 269.5839° |
| revolutions per day: | 15.27571224 |
| mean anomaly at epoch: | 90.4880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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