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 63968U 26145.34999001 +.00000000 +00000-0 +56346-3 0 00005
2 63968 43.0017 103.0058 0001633 258.4390 101.6279 15.27594564 04
| Epoch (UTC): | 25 May 2026 08:23:59 |
| Eccentricity: | 0.0001633 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 103.0058° |
| argument of perigee: | 258.4390° |
| revolutions per day: | 15.27594564 |
| mean anomaly at epoch: | 101.6279° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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