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 53754U 26145.47107119 +.00000000 +00000-0 +39209-3 0 00001
2 53754 53.2341 316.4765 0396764 162.4787 199.0339 14.69333597 00
| Epoch (UTC): | 25 May 2026 11:18:20 |
| Eccentricity: | 0.0396764 |
| inclination: | 53.2341° |
| perigee height: | 384 km |
| apogee height: | 943 km |
| right ascension of ascending node: | 316.4765° |
| argument of perigee: | 162.4787° |
| revolutions per day: | 14.69333597 |
| mean anomaly at epoch: | 199.0339° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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