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 63168U 26145.57343843 +.00000000 +00000-0 +61103-4 0 00007
2 63168 88.9691 302.9334 0013149 24.2414 335.9353 13.51007220 08
| Epoch (UTC): | 25 May 2026 13:45:45 |
| Eccentricity: | 0.0013149 |
| inclination: | 88.9691° |
| perigee height: | 1059 km |
| apogee height: | 1078 km |
| right ascension of ascending node: | 302.9334° |
| argument of perigee: | 24.2414° |
| revolutions per day: | 13.51007220 |
| mean anomaly at epoch: | 335.9353° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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