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 51721U 26145.56792617 +.00000000 +00000-0 -20123-4 0 00003
2 51721 53.2127 344.0105 0001457 93.1433 266.9725 15.08838850 08
| Epoch (UTC): | 25 May 2026 13:37:48 |
| Eccentricity: | 0.0001457 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 344.0105° |
| argument of perigee: | 93.1433° |
| revolutions per day: | 15.08838850 |
| mean anomaly at epoch: | 266.9725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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