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 58740U 26145.49067322 +.00000000 +00000-0 +52190-4 0 00009
2 58740 43.0010 145.6508 0001376 275.5685 84.5010 15.27581933 00
| Epoch (UTC): | 25 May 2026 11:46:34 |
| Eccentricity: | 0.0001376 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 145.6508° |
| argument of perigee: | 275.5685° |
| revolutions per day: | 15.27581933 |
| mean anomaly at epoch: | 84.5010° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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