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 63985U 26145.60935163 +.00000000 +00000-0 +78185-3 0 00007
2 63985 97.3671 221.6324 0008549 15.0290 345.1203 15.30735487 00
| Epoch (UTC): | 25 May 2026 14:37:27 |
| Eccentricity: | 0.0008549 |
| inclination: | 97.3671° |
| perigee height: | 468 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 221.6324° |
| argument of perigee: | 15.0290° |
| revolutions per day: | 15.30735487 |
| mean anomaly at epoch: | 345.1203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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