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 57088U 26145.01382861 +.00000000 +00000-0 +61335-4 0 00000
2 57088 43.0038 25.0383 0001584 262.8809 97.1862 15.27578777 01
| Epoch (UTC): | 25 May 2026 00:19:54 |
| Eccentricity: | 0.0001584 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 25.0383° |
| argument of perigee: | 262.8809° |
| revolutions per day: | 15.27578777 |
| mean anomaly at epoch: | 97.1862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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