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 53653U 26145.66668980 +.00000000 +00000-0 +21369-2 0 00005
2 53653 97.6037 27.6044 0001539 76.3913 289.2268 15.38099593 05
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001539 |
| inclination: | 97.6037° |
| perigee height: | 451 km |
| apogee height: | 453 km |
| right ascension of ascending node: | 27.6044° |
| argument of perigee: | 76.3913° |
| revolutions per day: | 15.38099593 |
| mean anomaly at epoch: | 289.2268° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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