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 56068U 26145.53668912 +.00000000 +00000-0 +42359-3 0 00002
2 56068 87.9262 248.4743 0001808 94.1797 265.9544 13.21825221 09
| Epoch (UTC): | 25 May 2026 12:52:49 |
| Eccentricity: | 0.0001808 |
| inclination: | 87.9262° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4743° |
| argument of perigee: | 94.1797° |
| revolutions per day: | 13.21825221 |
| mean anomaly at epoch: | 265.9544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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