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 63068U 26145.48701142 +.00000000 +00000-0 +55178-3 0 00000
2 63068 43.0017 73.4713 0000907 277.2390 82.8359 15.27593770 02
| Epoch (UTC): | 25 May 2026 11:41:17 |
| Eccentricity: | 0.0000907 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 73.4713° |
| argument of perigee: | 277.2390° |
| revolutions per day: | 15.27593770 |
| mean anomaly at epoch: | 82.8359° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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