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 56051U 26145.53330844 +.00000000 +00000-0 +37051-3 0 00007
2 56051 87.9253 248.4884 0001682 108.7012 251.4304 13.21827827 07
| Epoch (UTC): | 25 May 2026 12:47:57 |
| Eccentricity: | 0.0001682 |
| inclination: | 87.9253° |
| perigee height: | 1176 km |
| apogee height: | 1179 km |
| right ascension of ascending node: | 248.4884° |
| argument of perigee: | 108.7012° |
| revolutions per day: | 13.21827827 |
| mean anomaly at epoch: | 251.4304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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