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 57223U 26145.48942063 +.00000000 +00000-0 +18569-2 0 00007
2 57223 43.0030 320.1844 0000959 208.7725 151.3074 15.27307901 03
| Epoch (UTC): | 25 May 2026 11:44:45 |
| Eccentricity: | 0.0000959 |
| inclination: | 43.0030° |
| perigee height: | 483 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 320.1844° |
| argument of perigee: | 208.7725° |
| revolutions per day: | 15.27307901 |
| mean anomaly at epoch: | 151.3074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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