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 51870U 26145.66264904 +.00000000 +00000-0 -10762-4 0 00000
2 51870 53.2138 23.5755 0001564 85.1162 275.0009 15.08841642 03
| Epoch (UTC): | 25 May 2026 15:54:12 |
| Eccentricity: | 0.0001564 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 23.5755° |
| argument of perigee: | 85.1162° |
| revolutions per day: | 15.08841642 |
| mean anomaly at epoch: | 275.0009° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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