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 56102U 26145.52489878 +.00000000 +00000-0 +31607-4 0 00007
2 56102 43.0036 87.5240 0000999 270.1356 89.9381 15.27577879 05
| Epoch (UTC): | 25 May 2026 12:35:51 |
| Eccentricity: | 0.0000999 |
| inclination: | 43.0036° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.5240° |
| argument of perigee: | 270.1356° |
| revolutions per day: | 15.27577879 |
| mean anomaly at epoch: | 89.9381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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