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 63967U 26145.34616081 +.00000000 +00000-0 +75262-3 0 00006
2 63967 43.0029 102.9775 0001762 267.2036 92.8614 15.27584568 05
| Epoch (UTC): | 25 May 2026 08:18:28 |
| Eccentricity: | 0.0001762 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 102.9775° |
| argument of perigee: | 267.2036° |
| revolutions per day: | 15.27584568 |
| mean anomaly at epoch: | 92.8614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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