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 57375U 26145.36627623 +.00000000 +00000-0 +11700-4 0 00006
2 57375 43.0015 168.8401 0001100 278.3690 81.7037 15.27573547 09
| Epoch (UTC): | 25 May 2026 08:47:26 |
| Eccentricity: | 0.0001100 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 168.8401° |
| argument of perigee: | 278.3690° |
| revolutions per day: | 15.27573547 |
| mean anomaly at epoch: | 81.7037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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