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 53721U 26145.64560823 +.00000000 +00000-0 -25139-4 0 00008
2 53721 53.2105 268.4869 0001354 85.1143 275.0003 15.08843972 08
| Epoch (UTC): | 25 May 2026 15:29:40 |
| Eccentricity: | 0.0001354 |
| inclination: | 53.2105° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 268.4869° |
| argument of perigee: | 85.1143° |
| revolutions per day: | 15.08843972 |
| mean anomaly at epoch: | 275.0003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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