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 63765U 26145.50483354 +.00000000 +00000-0 +53072-3 0 00000
2 63765 42.9999 331.5800 0001138 259.1270 100.9454 15.27595622 07
| Epoch (UTC): | 25 May 2026 12:06:57 |
| Eccentricity: | 0.0001138 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.5800° |
| argument of perigee: | 259.1270° |
| revolutions per day: | 15.27595622 |
| mean anomaly at epoch: | 100.9454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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