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 63050U 26145.36787910 +.00000000 +00000-0 +68875-3 0 00003
2 63050 53.1580 274.2378 0000601 102.2219 257.8851 15.34405627 08
| Epoch (UTC): | 25 May 2026 08:49:44 |
| Eccentricity: | 0.0000601 |
| inclination: | 53.1580° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 274.2378° |
| argument of perigee: | 102.2219° |
| revolutions per day: | 15.34405627 |
| mean anomaly at epoch: | 257.8851° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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