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 51804U 26145.26152694 +.00000000 +00000-0 -50771-4 0 00009
2 51804 53.2134 345.3754 0001221 97.8921 262.2210 15.08831113 07
| Epoch (UTC): | 25 May 2026 06:16:35 |
| Eccentricity: | 0.0001221 |
| inclination: | 53.2134° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 345.3754° |
| argument of perigee: | 97.8921° |
| revolutions per day: | 15.08831113 |
| mean anomaly at epoch: | 262.2210° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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