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 57792U 26145.58944056 +.00000000 +00000-0 +18480-3 0 00006
2 57792 49.9722 247.3991 0013729 178.6125 181.4827 14.23108284 06
| Epoch (UTC): | 25 May 2026 14:08:47 |
| Eccentricity: | 0.0013729 |
| inclination: | 49.9722° |
| perigee height: | 805 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 247.3991° |
| argument of perigee: | 178.6125° |
| revolutions per day: | 14.23108284 |
| mean anomaly at epoch: | 181.4827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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