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 43180U 26145.54152336 +.00000000 +00000-0 +98792-4 0 00005
2 43180 97.3598 51.5214 0001962 81.4421 278.7038 15.22860030 07
| Epoch (UTC): | 25 May 2026 12:59:47 |
| Eccentricity: | 0.0001962 |
| inclination: | 97.3598° |
| perigee height: | 496 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 51.5214° |
| argument of perigee: | 81.4421° |
| revolutions per day: | 15.22860030 |
| mean anomaly at epoch: | 278.7038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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