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 57793U 26145.57291977 +.00000000 +00000-0 +80358-4 0 00007
2 57793 49.9684 247.6832 0013729 182.2357 177.8496 14.23107726 00
| Epoch (UTC): | 25 May 2026 13:45:00 |
| Eccentricity: | 0.0013729 |
| inclination: | 49.9684° |
| perigee height: | 805 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 247.6832° |
| argument of perigee: | 182.2357° |
| revolutions per day: | 14.23107726 |
| mean anomaly at epoch: | 177.8496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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