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 53165U 26145.39262720 +.00000000 +00000-0 -12455-3 0 00003
2 53165 53.2110 179.7873 0001256 94.5242 265.5894 15.08849026 08
| Epoch (UTC): | 25 May 2026 09:25:22 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.2110° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 179.7873° |
| argument of perigee: | 94.5242° |
| revolutions per day: | 15.08849026 |
| mean anomaly at epoch: | 265.5894° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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