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 57045U 26144.75709683 +.00000000 +00000-0 +00000-0 0 00006
2 57045 0.0383 333.9910 0004025 11.0302 315.8823 1.00268796 02
| Epoch (UTC): | 24 May 2026 18:10:13 |
| Eccentricity: | 0.0004025 |
| inclination: | 0.0383° |
| perigee height: | 35770 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 333.9910° |
| argument of perigee: | 11.0302° |
| revolutions per day: | 1.00268796 |
| mean anomaly at epoch: | 315.8823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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