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 63640U 26145.13420477 +.00000000 +00000-0 +38583-3 0 00008
2 63640 42.9993 293.8783 0001198 268.1518 91.9196 15.27591646 08
| Epoch (UTC): | 25 May 2026 03:13:15 |
| Eccentricity: | 0.0001198 |
| inclination: | 42.9993° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 293.8783° |
| argument of perigee: | 268.1518° |
| revolutions per day: | 15.27591646 |
| mean anomaly at epoch: | 91.9196° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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