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 63861U 26145.01611419 +.00000000 +00000-0 +55517-3 0 00004
2 63861 43.0032 6.9748 0001415 265.9370 94.1320 15.27588586 09
| Epoch (UTC): | 25 May 2026 00:23:12 |
| Eccentricity: | 0.0001415 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 6.9748° |
| argument of perigee: | 265.9370° |
| revolutions per day: | 15.27588586 |
| mean anomaly at epoch: | 94.1320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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