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 53161U 26145.46990880 +.00000000 +00000-0 +90512-5 0 00003
2 53161 53.2111 179.4386 0001146 64.1773 295.9337 15.08838007 07
| Epoch (UTC): | 25 May 2026 11:16:40 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.4386° |
| argument of perigee: | 64.1773° |
| revolutions per day: | 15.08838007 |
| mean anomaly at epoch: | 295.9337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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