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 59773U 26145.73171964 +.00000000 +00000-0 +32415-3 0 00008
2 59773 97.4355 262.0276 0014309 92.4105 267.8769 15.19613541 00
| Epoch (UTC): | 25 May 2026 17:33:40 |
| Eccentricity: | 0.0014309 |
| inclination: | 97.4355° |
| perigee height: | 497 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 262.0276° |
| argument of perigee: | 92.4105° |
| revolutions per day: | 15.19613541 |
| mean anomaly at epoch: | 267.8769° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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