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 51141U 26145.47404561 +.00000000 +00000-0 +35047-4 0 00007
2 51141 53.2144 314.4215 0001315 86.1655 273.9487 15.08840421 07
| Epoch (UTC): | 25 May 2026 11:22:37 |
| Eccentricity: | 0.0001315 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 314.4215° |
| argument of perigee: | 86.1655° |
| revolutions per day: | 15.08840421 |
| mean anomaly at epoch: | 273.9487° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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