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 57514U 26145.63405052 +.00000000 +00000-0 +80674-4 0 00007
2 57514 43.0031 301.4516 0001575 261.7356 98.3317 15.27582293 08
| Epoch (UTC): | 25 May 2026 15:13:01 |
| Eccentricity: | 0.0001575 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 301.4516° |
| argument of perigee: | 261.7356° |
| revolutions per day: | 15.27582293 |
| mean anomaly at epoch: | 98.3317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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