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 63293U 26145.61908389 +.00000000 +00000-0 +39183-3 0 00005
2 63293 97.6481 286.3666 0042421 215.9981 143.8389 15.09849604 07
| Epoch (UTC): | 25 May 2026 14:51:28 |
| Eccentricity: | 0.0042421 |
| inclination: | 97.6481° |
| perigee height: | 507 km |
| apogee height: | 566 km |
| right ascension of ascending node: | 286.3666° |
| argument of perigee: | 215.9981° |
| revolutions per day: | 15.09849604 |
| mean anomaly at epoch: | 143.8389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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