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 54042U 26145.63211567 +.00000000 +00000-0 +44246-3 0 00000
2 54042 35.0060 261.6185 0028307 352.7023 7.3277 15.23332907 03
| Epoch (UTC): | 25 May 2026 15:10:14 |
| Eccentricity: | 0.0028307 |
| inclination: | 35.0060° |
| perigee height: | 476 km |
| apogee height: | 515 km |
| right ascension of ascending node: | 261.6185° |
| argument of perigee: | 352.7023° |
| revolutions per day: | 15.23332907 |
| mean anomaly at epoch: | 7.3277° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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