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 63243U 26145.38298735 +.00000000 +00000-0 +56948-3 0 00009
2 63243 97.3919 40.4366 0004540 168.1106 192.0242 15.29452797 08
| Epoch (UTC): | 25 May 2026 09:11:30 |
| Eccentricity: | 0.0004540 |
| inclination: | 97.3919° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 40.4366° |
| argument of perigee: | 168.1106° |
| revolutions per day: | 15.29452797 |
| mean anomaly at epoch: | 192.0242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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