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 63899U 26145.36928949 +.00000000 +00000-0 +36424-3 0 00008
2 63899 42.9989 103.2854 0000915 263.6580 96.4168 15.27591007 07
| Epoch (UTC): | 25 May 2026 08:51:46 |
| Eccentricity: | 0.0000915 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.2854° |
| argument of perigee: | 263.6580° |
| revolutions per day: | 15.27591007 |
| mean anomaly at epoch: | 96.4168° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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