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 63056U 26145.65431816 +.00000000 +00000-0 +13538-2 0 00007
2 63056 43.0025 271.5767 0000750 136.6419 223.4508 15.70953080 05
| Epoch (UTC): | 25 May 2026 15:42:13 |
| Eccentricity: | 0.0000750 |
| inclination: | 43.0025° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 271.5767° |
| argument of perigee: | 136.6419° |
| revolutions per day: | 15.70953080 |
| mean anomaly at epoch: | 223.4508° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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