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 63784U 26145.52923206 +.00000000 +00000-0 +89498-3 0 00009
2 63784 42.9979 331.6404 0000810 271.7985 88.2774 15.27592421 03
| Epoch (UTC): | 25 May 2026 12:42:05 |
| Eccentricity: | 0.0000810 |
| inclination: | 42.9979° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.6404° |
| argument of perigee: | 271.7985° |
| revolutions per day: | 15.27592421 |
| mean anomaly at epoch: | 88.2774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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