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 57768U 26145.42939343 +.00000000 +00000-0 +96010-4 0 00001
2 57768 80.9966 28.8197 0006905 73.9918 286.1999 13.85419047 01
| Epoch (UTC): | 25 May 2026 10:18:19 |
| Eccentricity: | 0.0006905 |
| inclination: | 80.9966° |
| perigee height: | 940 km |
| apogee height: | 950 km |
| right ascension of ascending node: | 28.8197° |
| argument of perigee: | 73.9918° |
| revolutions per day: | 13.85419047 |
| mean anomaly at epoch: | 286.1999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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