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 63851U 26145.57889226 +.00000000 +00000-0 +53837-3 0 00000
2 63851 43.0060 3.4777 0001103 267.6939 92.3787 15.27589428 00
| Epoch (UTC): | 25 May 2026 13:53:36 |
| Eccentricity: | 0.0001103 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.4777° |
| argument of perigee: | 267.6939° |
| revolutions per day: | 15.27589428 |
| mean anomaly at epoch: | 92.3787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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