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 56081U 26145.37448902 +.00000000 +00000-0 +85808-4 0 00001
2 56081 87.8988 263.7474 0001861 116.1778 243.9544 13.15549844 05
| Epoch (UTC): | 25 May 2026 08:59:15 |
| Eccentricity: | 0.0001861 |
| inclination: | 87.8988° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 263.7474° |
| argument of perigee: | 116.1778° |
| revolutions per day: | 13.15549844 |
| mean anomaly at epoch: | 243.9544° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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