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 63375U 26145.47973064 +.00000000 +00000-0 +69587-3 0 00003
2 63375 53.1598 53.1253 0001342 98.7760 261.3393 15.30203395 01
| Epoch (UTC): | 25 May 2026 11:30:48 |
| Eccentricity: | 0.0001342 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.1253° |
| argument of perigee: | 98.7760° |
| revolutions per day: | 15.30203395 |
| mean anomaly at epoch: | 261.3393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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