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 57124U 26145.19181497 +.00000000 +00000-0 +32183-4 0 00001
2 57124 43.0028 209.3989 0001479 274.5689 85.4994 15.26739422 00
| Epoch (UTC): | 25 May 2026 04:36:12 |
| Eccentricity: | 0.0001479 |
| inclination: | 43.0028° |
| perigee height: | 485 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 209.3989° |
| argument of perigee: | 274.5689° |
| revolutions per day: | 15.26739422 |
| mean anomaly at epoch: | 85.4994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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