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 63057U 26145.38408244 +.00000000 +00000-0 +18950-2 0 00000
2 63057 42.9986 272.9851 0001592 262.6789 97.3898 15.70853406 05
| Epoch (UTC): | 25 May 2026 09:13:04 |
| Eccentricity: | 0.0001592 |
| inclination: | 42.9986° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 272.9851° |
| argument of perigee: | 262.6789° |
| revolutions per day: | 15.70853406 |
| mean anomaly at epoch: | 97.3898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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