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 51720U 26145.55687909 +.00000000 +00000-0 -90917-4 0 00006
2 51720 53.2136 344.0203 0001365 89.3979 270.7169 15.08847705 00
| Epoch (UTC): | 25 May 2026 13:21:54 |
| Eccentricity: | 0.0001365 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.0203° |
| argument of perigee: | 89.3979° |
| revolutions per day: | 15.08847705 |
| mean anomaly at epoch: | 270.7169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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