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 51892U 26145.06004727 +.00000000 +00000-0 +16122-4 0 00008
2 51892 53.2151 16.2807 0001668 93.4585 266.6598 15.08835891 03
| Epoch (UTC): | 25 May 2026 01:26:28 |
| Eccentricity: | 0.0001668 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 16.2807° |
| argument of perigee: | 93.4585° |
| revolutions per day: | 15.08835891 |
| mean anomaly at epoch: | 266.6598° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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