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 39768U 26145.60987169 +.00000000 +00000-0 +16089-3 0 00007
2 39768 97.9054 258.8970 0007319 62.2596 297.9365 14.94690722 03
| Epoch (UTC): | 25 May 2026 14:38:12 |
| Eccentricity: | 0.0007319 |
| inclination: | 97.9054° |
| perigee height: | 578 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 258.8970° |
| argument of perigee: | 62.2596° |
| revolutions per day: | 14.94690722 |
| mean anomaly at epoch: | 297.9365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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