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 53623U 26145.57385431 +.00000000 +00000-0 +11197-3 0 00008
2 53623 53.2155 248.8493 0001192 87.9218 272.1911 15.08830302 01
| Epoch (UTC): | 25 May 2026 13:46:21 |
| Eccentricity: | 0.0001192 |
| inclination: | 53.2155° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 248.8493° |
| argument of perigee: | 87.9218° |
| revolutions per day: | 15.08830302 |
| mean anomaly at epoch: | 272.1911° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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