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 63388U 26145.43656664 +.00000000 +00000-0 +57561-3 0 00006
2 63388 53.1575 53.5680 0000880 65.0643 295.0449 15.30183372 09
| Epoch (UTC): | 25 May 2026 10:28:39 |
| Eccentricity: | 0.0000880 |
| inclination: | 53.1575° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.5680° |
| argument of perigee: | 65.0643° |
| revolutions per day: | 15.30183372 |
| mean anomaly at epoch: | 295.0449° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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