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 57365U 26145.54830045 +.00000000 +00000-0 +81342-5 0 00009
2 57365 43.0030 167.6247 0001305 265.8964 94.1739 15.27576027 05
| Epoch (UTC): | 25 May 2026 13:09:33 |
| Eccentricity: | 0.0001305 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.6247° |
| argument of perigee: | 265.8964° |
| revolutions per day: | 15.27576027 |
| mean anomaly at epoch: | 94.1739° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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