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 57104U 26145.53562102 +.00000000 +00000-0 -87214-4 0 00009
2 57104 43.0019 207.6853 0001398 281.1419 78.9276 15.27576842 00
| Epoch (UTC): | 25 May 2026 12:51:17 |
| Eccentricity: | 0.0001398 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 207.6853° |
| argument of perigee: | 281.1419° |
| revolutions per day: | 15.27576842 |
| mean anomaly at epoch: | 78.9276° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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