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 57147U 26145.47636469 +.00000000 +00000-0 +72978-4 0 00007
2 57147 43.0008 189.9600 0001225 273.1975 86.8736 15.27581015 01
| Epoch (UTC): | 25 May 2026 11:25:57 |
| Eccentricity: | 0.0001225 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 189.9600° |
| argument of perigee: | 273.1975° |
| revolutions per day: | 15.27581015 |
| mean anomaly at epoch: | 86.8736° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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