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 63117U 26145.58335647 +.00000000 +00000-0 +19377-2 0 00009
2 63117 42.9925 284.6421 0024005 335.7056 119.4642 15.55682252 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0024005 |
| inclination: | 42.9925° |
| perigee height: | 384 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 284.6421° |
| argument of perigee: | 335.7056° |
| revolutions per day: | 15.55682252 |
| mean anomaly at epoch: | 119.4642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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