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 53160U 26145.35951866 +.00000000 +00000-0 +91581-4 0 00007
2 53160 53.2142 179.9353 0001161 75.0738 285.0382 15.08838916 07
| Epoch (UTC): | 25 May 2026 08:37:42 |
| Eccentricity: | 0.0001161 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.9353° |
| argument of perigee: | 75.0738° |
| revolutions per day: | 15.08838916 |
| mean anomaly at epoch: | 285.0382° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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