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 56803U 26145.41550141 +.00000000 +00000-0 +49510-4 0 00007
2 56803 69.9984 150.9774 0003682 267.9804 92.0933 14.98321151 08
| Epoch (UTC): | 25 May 2026 09:58:19 |
| Eccentricity: | 0.0003682 |
| inclination: | 69.9984° |
| perigee height: | 570 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.9774° |
| argument of perigee: | 267.9804° |
| revolutions per day: | 14.98321151 |
| mean anomaly at epoch: | 92.0933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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