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 25544U 26141.16510469 +.00000000 +00000-0 +11282-3 0 00006
2 25544 51.6328 73.8715 0007529 81.3651 278.8190 15.49291753 06
| Epoch (UTC): | 21 May 2026 03:57:45 |
| Eccentricity: | 0.0007529 |
| inclination: | 51.6328° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 73.8715° |
| argument of perigee: | 81.3651° |
| revolutions per day: | 15.49291753 |
| mean anomaly at epoch: | 278.8190° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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