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 51104U 26145.18056684 +.00000000 +00000-0 +20964-4 0 00005
2 51104 53.2148 305.7401 0001304 82.5095 277.6045 15.08838819 05
| Epoch (UTC): | 25 May 2026 04:20:00 |
| Eccentricity: | 0.0001304 |
| inclination: | 53.2148° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 305.7401° |
| argument of perigee: | 82.5095° |
| revolutions per day: | 15.08838819 |
| mean anomaly at epoch: | 277.6045° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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