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 56901U 26145.61701719 +.00000000 +00000-0 -25963-4 0 00004
2 56901 42.9906 7.4761 0002975 141.2287 218.8778 15.27561422 02
| Epoch (UTC): | 25 May 2026 14:48:30 |
| Eccentricity: | 0.0002975 |
| inclination: | 42.9906° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 7.4761° |
| argument of perigee: | 141.2287° |
| revolutions per day: | 15.27561422 |
| mean anomaly at epoch: | 218.8778° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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