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 63901U 26145.36157808 +.00000000 +00000-0 +60857-3 0 00007
2 63901 43.0000 103.2252 0001716 268.3999 91.6656 15.27594232 07
| Epoch (UTC): | 25 May 2026 08:40:40 |
| Eccentricity: | 0.0001716 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2252° |
| argument of perigee: | 268.3999° |
| revolutions per day: | 15.27594232 |
| mean anomaly at epoch: | 91.6656° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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