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 57956U 26145.37615802 +.00000000 +00000-0 +63966-3 0 00008
2 57956 97.6067 302.4301 0002415 292.5905 67.5105 15.76525579 02
| Epoch (UTC): | 25 May 2026 09:01:40 |
| Eccentricity: | 0.0002415 |
| inclination: | 97.6067° |
| perigee height: | 339 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 302.4301° |
| argument of perigee: | 292.5905° |
| revolutions per day: | 15.76525579 |
| mean anomaly at epoch: | 67.5105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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