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 63989U 26145.63469465 +.00000000 +00000-0 +82478-3 0 00001
2 63989 97.3689 222.1506 0007817 17.2347 342.9160 15.34239539 03
| Epoch (UTC): | 25 May 2026 15:13:57 |
| Eccentricity: | 0.0007817 |
| inclination: | 97.3689° |
| perigee height: | 458 km |
| apogee height: | 469 km |
| right ascension of ascending node: | 222.1506° |
| argument of perigee: | 17.2347° |
| revolutions per day: | 15.34239539 |
| mean anomaly at epoch: | 342.9160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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