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 64863U 26145.39938286 +.00000000 +00000-0 +27923-3 0 00002
2 64863 97.4496 0.7970 0002162 80.3834 279.7637 15.05657257 02
| Epoch (UTC): | 25 May 2026 09:35:06 |
| Eccentricity: | 0.0002162 |
| inclination: | 97.4496° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7970° |
| argument of perigee: | 80.3834° |
| revolutions per day: | 15.05657257 |
| mean anomaly at epoch: | 279.7637° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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