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 53416U 26145.38250005 +.00000000 +00000-0 +48998-4 0 00005
2 53416 53.2150 129.7812 0001108 83.0929 277.0189 15.08839059 00
| Epoch (UTC): | 25 May 2026 09:10:48 |
| Eccentricity: | 0.0001108 |
| inclination: | 53.2150° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 129.7812° |
| argument of perigee: | 83.0929° |
| revolutions per day: | 15.08839059 |
| mean anomaly at epoch: | 277.0189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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