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 51714U 26145.25146279 +.00000000 +00000-0 +63821-4 0 00009
2 51714 53.2132 345.3969 0001628 115.6957 244.4203 15.08829845 05
| Epoch (UTC): | 25 May 2026 06:02:06 |
| Eccentricity: | 0.0001628 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 345.3969° |
| argument of perigee: | 115.6957° |
| revolutions per day: | 15.08829845 |
| mean anomaly at epoch: | 244.4203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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