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 63969U 26145.60382524 +.00000000 +00000-0 +67028-3 0 00000
2 63969 43.0007 101.4708 0001518 273.6112 86.4566 15.27589263 00
| Epoch (UTC): | 25 May 2026 14:29:30 |
| Eccentricity: | 0.0001518 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 101.4708° |
| argument of perigee: | 273.6112° |
| revolutions per day: | 15.27589263 |
| mean anomaly at epoch: | 86.4566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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