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 51117U 26145.42711485 +.00000000 +00000-0 +50904-4 0 00000
2 51117 53.2126 304.5224 0001259 87.4798 272.6338 15.08839493 07
| Epoch (UTC): | 25 May 2026 10:15:02 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 304.5224° |
| argument of perigee: | 87.4798° |
| revolutions per day: | 15.08839493 |
| mean anomaly at epoch: | 272.6338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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