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 53886U 26144.94735661 +.00000000 +00000-0 +22375-3 0 00003
2 53886 53.2169 342.0145 0001076 55.7913 304.3181 15.08863527 06
| Epoch (UTC): | 24 May 2026 22:44:11 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.2169° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 342.0145° |
| argument of perigee: | 55.7913° |
| revolutions per day: | 15.08863527 |
| mean anomaly at epoch: | 304.3181° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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