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 63916U 26145.26792594 +.00000000 +00000-0 +66590-3 0 00009
2 63916 42.9990 103.3780 0000059 5.3923 354.6929 15.27595946 09
| Epoch (UTC): | 25 May 2026 06:25:48 |
| Eccentricity: | 0.0000059 |
| inclination: | 42.9990° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 103.3780° |
| argument of perigee: | 5.3923° |
| revolutions per day: | 15.27595946 |
| mean anomaly at epoch: | 354.6929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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