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 25774U 26075.14534006 +.00000000 +00000-0 +45397-4 0 00003
2 25774 51.5288 232.5850 0373946 263.4125 272.4627 13.46768238 04
| Epoch (UTC): | 16 March 2026 03:29:17 |
| Eccentricity: | 0.0373946 |
| inclination: | 51.5288° |
| perigee height: | 805 km |
| apogee height: | 1363 km |
| right ascension of ascending node: | 232.5850° |
| argument of perigee: | 263.4125° |
| revolutions per day: | 13.46768238 |
| mean anomaly at epoch: | 272.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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