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 63062U 26145.64370035 +.00000000 +00000-0 +15724-2 0 00007
2 63062 42.9986 271.4921 0002581 251.9785 108.0801 15.70980994 06
| Epoch (UTC): | 25 May 2026 15:26:55 |
| Eccentricity: | 0.0002581 |
| inclination: | 42.9986° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 271.4921° |
| argument of perigee: | 251.9785° |
| revolutions per day: | 15.70980994 |
| mean anomaly at epoch: | 108.0801° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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