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 53692U 26145.40323943 +.00000000 +00000-0 +12106-2 0 00006
2 53692 97.6101 33.4348 0002604 78.9815 281.1715 15.25234306 02
| Epoch (UTC): | 25 May 2026 09:40:39 |
| Eccentricity: | 0.0002604 |
| inclination: | 97.6101° |
| perigee height: | 488 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 33.4348° |
| argument of perigee: | 78.9815° |
| revolutions per day: | 15.25234306 |
| mean anomaly at epoch: | 281.1715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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