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 63145U 26145.48285494 +.00000000 +00000-0 +60607-3 0 00006
2 63145 42.9992 302.8201 0001179 276.6368 83.4349 15.27593981 09
| Epoch (UTC): | 25 May 2026 11:35:18 |
| Eccentricity: | 0.0001179 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 302.8201° |
| argument of perigee: | 276.6368° |
| revolutions per day: | 15.27593981 |
| mean anomaly at epoch: | 83.4349° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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