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 57932U 26145.59548808 +.00000000 +00000-0 +96964-5 0 00003
2 57932 42.9999 250.5509 0000908 271.1492 88.9255 15.27577609 05
| Epoch (UTC): | 25 May 2026 14:17:30 |
| Eccentricity: | 0.0000908 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 250.5509° |
| argument of perigee: | 271.1492° |
| revolutions per day: | 15.27577609 |
| mean anomaly at epoch: | 88.9255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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