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 57339U 26145.57513632 +.00000000 +00000-0 +27496-4 0 00002
2 57339 43.0012 178.3115 0000241 183.7972 176.2877 15.27576494 07
| Epoch (UTC): | 25 May 2026 13:48:11 |
| Eccentricity: | 0.0000241 |
| inclination: | 43.0012° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 178.3115° |
| argument of perigee: | 183.7972° |
| revolutions per day: | 15.27576494 |
| mean anomaly at epoch: | 176.2877° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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