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 63997U 26145.09268375 +.00000000 +00000-0 +53556-3 0 00002
2 63997 42.9955 286.1734 0000792 303.1001 56.9775 15.27599516 06
| Epoch (UTC): | 25 May 2026 02:13:27 |
| Eccentricity: | 0.0000792 |
| inclination: | 42.9955° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 286.1734° |
| argument of perigee: | 303.1001° |
| revolutions per day: | 15.27599516 |
| mean anomaly at epoch: | 56.9775° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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