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 53601U 26145.57293234 +.00000000 +00000-0 +32077-4 0 00004
2 53601 53.2162 258.8352 0001271 83.0013 277.1124 15.08839092 04
| Epoch (UTC): | 25 May 2026 13:45:01 |
| Eccentricity: | 0.0001271 |
| inclination: | 53.2162° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 258.8352° |
| argument of perigee: | 83.0013° |
| revolutions per day: | 15.08839092 |
| mean anomaly at epoch: | 277.1124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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