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 57143U 26145.57116053 +.00000000 +00000-0 +16427-4 0 00003
2 57143 43.0031 188.9677 0001978 301.8171 58.2488 15.27576225 02
| Epoch (UTC): | 25 May 2026 13:42:28 |
| Eccentricity: | 0.0001978 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 188.9677° |
| argument of perigee: | 301.8171° |
| revolutions per day: | 15.27576225 |
| mean anomaly at epoch: | 58.2488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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