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 63659U 26145.42211892 +.00000000 +00000-0 +91020-3 0 00004
2 63659 42.9940 295.2660 0000625 90.9226 269.1697 15.27612492 09
| Epoch (UTC): | 25 May 2026 10:07:51 |
| Eccentricity: | 0.0000625 |
| inclination: | 42.9940° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 295.2660° |
| argument of perigee: | 90.9226° |
| revolutions per day: | 15.27612492 |
| mean anomaly at epoch: | 269.1697° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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