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 56053U 26145.56620677 +.00000000 +00000-0 +20623-3 0 00005
2 56053 87.8990 263.7341 0001588 104.1423 255.9884 13.15547926 09
| Epoch (UTC): | 25 May 2026 13:35:20 |
| Eccentricity: | 0.0001588 |
| inclination: | 87.8990° |
| perigee height: | 1201 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7341° |
| argument of perigee: | 104.1423° |
| revolutions per day: | 13.15547926 |
| mean anomaly at epoch: | 255.9884° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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