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 51130U 26145.18701289 +.00000000 +00000-0 +42613-4 0 00007
2 51130 53.2130 315.7113 0001361 89.1876 270.9272 15.08835265 09
| Epoch (UTC): | 25 May 2026 04:29:17 |
| Eccentricity: | 0.0001361 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 315.7113° |
| argument of perigee: | 89.1876° |
| revolutions per day: | 15.08835265 |
| mean anomaly at epoch: | 270.9272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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