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 53964U 26145.55272654 +.00000000 +00000-0 -77946-5 0 00003
2 53964 53.2117 239.2239 0001468 86.1308 273.9852 15.08839219 05
| Epoch (UTC): | 25 May 2026 13:15:55 |
| Eccentricity: | 0.0001468 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 239.2239° |
| argument of perigee: | 86.1308° |
| revolutions per day: | 15.08839219 |
| mean anomaly at epoch: | 273.9852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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