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 63420U 26145.39063205 +.00000000 +00000-0 +91442-3 0 00007
2 63420 43.0000 33.5615 0001770 269.5116 90.5533 15.27589294 09
| Epoch (UTC): | 25 May 2026 09:22:30 |
| Eccentricity: | 0.0001770 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 33.5615° |
| argument of perigee: | 269.5116° |
| revolutions per day: | 15.27589294 |
| mean anomaly at epoch: | 90.5533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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