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 57208U 26145.57875931 +.00000000 +00000-0 +50219-3 0 00008
2 57208 97.5102 216.0290 0007826 141.2437 218.9370 15.37846809 04
| Epoch (UTC): | 25 May 2026 13:53:24 |
| Eccentricity: | 0.0007826 |
| inclination: | 97.5102° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 216.0290° |
| argument of perigee: | 141.2437° |
| revolutions per day: | 15.37846809 |
| mean anomaly at epoch: | 218.9370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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