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 63993U 26145.63586727 +.00000000 +00000-0 +83554-3 0 00003
2 63993 97.3664 222.0345 0009194 37.6518 322.5366 15.33942150 08
| Epoch (UTC): | 25 May 2026 15:15:38 |
| Eccentricity: | 0.0009194 |
| inclination: | 97.3664° |
| perigee height: | 458 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 222.0345° |
| argument of perigee: | 37.6518° |
| revolutions per day: | 15.33942150 |
| mean anomaly at epoch: | 322.5366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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