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 63810U 26144.91455772 +.00000000 +00000-0 +51583-3 0 00003
2 63810 42.9993 101.9502 0000748 259.9732 100.1035 15.27586146 05
| Epoch (UTC): | 24 May 2026 21:56:57 |
| Eccentricity: | 0.0000748 |
| inclination: | 42.9993° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 101.9502° |
| argument of perigee: | 259.9732° |
| revolutions per day: | 15.27586146 |
| mean anomaly at epoch: | 100.1035° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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