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 63135U 26145.46256529 +.00000000 +00000-0 +20799-2 0 00007
2 63135 43.0007 148.2120 0001603 270.1030 89.9654 15.70926158 00
| Epoch (UTC): | 25 May 2026 11:06:05 |
| Eccentricity: | 0.0001603 |
| inclination: | 43.0007° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 148.2120° |
| argument of perigee: | 270.1030° |
| revolutions per day: | 15.70926158 |
| mean anomaly at epoch: | 89.9654° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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