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 57642U 26145.34501940 +.00000000 +00000-0 -17110-4 0 00006
2 57642 43.0044 19.3147 0000800 300.9406 59.1367 15.27583480 00
| Epoch (UTC): | 25 May 2026 08:16:49 |
| Eccentricity: | 0.0000800 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 19.3147° |
| argument of perigee: | 300.9406° |
| revolutions per day: | 15.27583480 |
| mean anomaly at epoch: | 59.1367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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