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 56725U 26145.36647144 +.00000000 +00000-0 +25429-4 0 00007
2 56725 86.6758 92.7992 0001973 80.7568 279.3788 13.22468027 08
| Epoch (UTC): | 25 May 2026 08:47:43 |
| Eccentricity: | 0.0001973 |
| inclination: | 86.6758° |
| perigee height: | 1174 km |
| apogee height: | 1177 km |
| right ascension of ascending node: | 92.7992° |
| argument of perigee: | 80.7568° |
| revolutions per day: | 13.22468027 |
| mean anomaly at epoch: | 279.3788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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