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 57092U 26145.06250412 +.00000000 +00000-0 +89505-4 0 00005
2 57092 43.0069 24.5488 0001670 278.8556 81.2106 15.27576633 06
| Epoch (UTC): | 25 May 2026 01:30:00 |
| Eccentricity: | 0.0001670 |
| inclination: | 43.0069° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 24.5488° |
| argument of perigee: | 278.8556° |
| revolutions per day: | 15.27576633 |
| mean anomaly at epoch: | 81.2106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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