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 57089U 26145.00869657 +.00000000 +00000-0 +18094-3 0 00006
2 57089 43.0028 24.9990 0001679 262.4039 97.6622 15.27585150 01
| Epoch (UTC): | 25 May 2026 00:12:31 |
| Eccentricity: | 0.0001679 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 24.9990° |
| argument of perigee: | 262.4039° |
| revolutions per day: | 15.27585150 |
| mean anomaly at epoch: | 97.6622° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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