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 51640U 26145.41615512 +.00000000 +00000-0 -90357-3 0 00000
2 51640 87.8849 40.8173 0001732 84.1962 275.9363 13.10371409 02
| Epoch (UTC): | 25 May 2026 09:59:15 |
| Eccentricity: | 0.0001732 |
| inclination: | 87.8849° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.8173° |
| argument of perigee: | 84.1962° |
| revolutions per day: | 13.10371409 |
| mean anomaly at epoch: | 275.9363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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