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 63795U 26144.95263936 +.00000000 +00000-0 +10429-2 0 00001
2 63795 43.0018 342.0044 0001694 261.5106 98.5554 15.27598121 03
| Epoch (UTC): | 24 May 2026 22:51:48 |
| Eccentricity: | 0.0001694 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.0044° |
| argument of perigee: | 261.5106° |
| revolutions per day: | 15.27598121 |
| mean anomaly at epoch: | 98.5554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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