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 63639U 26145.43415311 +.00000000 +00000-0 +81675-3 0 00000
2 63639 42.9993 291.8161 0000915 280.6000 79.4749 15.27594684 05
| Epoch (UTC): | 25 May 2026 10:25:10 |
| Eccentricity: | 0.0000915 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.8161° |
| argument of perigee: | 280.6000° |
| revolutions per day: | 15.27594684 |
| mean anomaly at epoch: | 79.4749° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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