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 63777U 26144.92532800 +.00000000 +00000-0 +54893-3 0 00001
2 63777 43.0029 334.8393 0001891 285.5138 74.5505 15.27599215 06
| Epoch (UTC): | 24 May 2026 22:12:28 |
| Eccentricity: | 0.0001891 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 334.8393° |
| argument of perigee: | 285.5138° |
| revolutions per day: | 15.27599215 |
| mean anomaly at epoch: | 74.5505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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