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 57240U 26145.51177757 +.00000000 +00000-0 +50214-4 0 00005
2 57240 43.0033 305.6373 0001892 266.6714 93.3921 15.27576103 06
| Epoch (UTC): | 25 May 2026 12:16:57 |
| Eccentricity: | 0.0001892 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 305.6373° |
| argument of perigee: | 266.6714° |
| revolutions per day: | 15.27576103 |
| mean anomaly at epoch: | 93.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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