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 63781U 26145.54369751 +.00000000 +00000-0 +11481-2 0 00003
2 63781 42.9997 338.7020 0001595 254.3183 105.7493 15.27619721 06
| Epoch (UTC): | 25 May 2026 13:02:55 |
| Eccentricity: | 0.0001595 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 338.7020° |
| argument of perigee: | 254.3183° |
| revolutions per day: | 15.27619721 |
| mean anomaly at epoch: | 105.7493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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