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 57763U 26145.42734094 +.00000000 +00000-0 +11976-3 0 00009
2 57763 80.9968 28.9954 0006859 77.6557 282.5366 13.85340645 03
| Epoch (UTC): | 25 May 2026 10:15:22 |
| Eccentricity: | 0.0006859 |
| inclination: | 80.9968° |
| perigee height: | 940 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 28.9954° |
| argument of perigee: | 77.6557° |
| revolutions per day: | 13.85340645 |
| mean anomaly at epoch: | 282.5366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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