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 63181U 26145.50106369 +.00000000 +00000-0 +76832-4 0 00000
2 63181 97.9566 331.0229 0008020 252.6084 107.4248 14.74321186 03
| Epoch (UTC): | 25 May 2026 12:01:31 |
| Eccentricity: | 0.0008020 |
| inclination: | 97.9566° |
| perigee height: | 642 km |
| apogee height: | 653 km |
| right ascension of ascending node: | 331.0229° |
| argument of perigee: | 252.6084° |
| revolutions per day: | 14.74321186 |
| mean anomaly at epoch: | 107.4248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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