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 63986U 26145.62057052 +.00000000 +00000-0 +61153-3 0 00009
2 63986 97.3633 218.8865 0013152 46.8777 313.3557 15.20666680 01
| Epoch (UTC): | 25 May 2026 14:53:37 |
| Eccentricity: | 0.0013152 |
| inclination: | 97.3633° |
| perigee height: | 495 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 218.8865° |
| argument of perigee: | 46.8777° |
| revolutions per day: | 15.20666680 |
| mean anomaly at epoch: | 313.3557° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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