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 57501U 26145.13794484 +.00000000 +00000-0 +46272-5 0 00005
2 57501 43.0013 304.6009 0001387 273.9639 86.1054 15.27581592 00
| Epoch (UTC): | 25 May 2026 03:18:38 |
| Eccentricity: | 0.0001387 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 304.6009° |
| argument of perigee: | 273.9639° |
| revolutions per day: | 15.27581592 |
| mean anomaly at epoch: | 86.1054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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