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 56960U 26145.56485662 +.00000000 +00000-0 +23779-3 0 00000
2 56960 97.6238 285.6373 0008942 59.5901 300.6224 15.34251811 07
| Epoch (UTC): | 25 May 2026 13:33:23 |
| Eccentricity: | 0.0008942 |
| inclination: | 97.6238° |
| perigee height: | 457 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 285.6373° |
| argument of perigee: | 59.5901° |
| revolutions per day: | 15.34251811 |
| mean anomaly at epoch: | 300.6224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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