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 63149U 26144.85839731 +.00000000 +00000-0 +54519-3 0 00004
2 63149 42.9970 305.8798 0001748 271.6528 88.4123 15.27602500 01
| Epoch (UTC): | 24 May 2026 20:36:05 |
| Eccentricity: | 0.0001748 |
| inclination: | 42.9970° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 305.8798° |
| argument of perigee: | 271.6528° |
| revolutions per day: | 15.27602500 |
| mean anomaly at epoch: | 88.4123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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