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 58439U 26145.52452071 +.00000000 +00000-0 +25541-3 0 00006
2 58439 43.0014 327.8337 0001335 275.5929 84.4770 15.27586469 00
| Epoch (UTC): | 25 May 2026 12:35:18 |
| Eccentricity: | 0.0001335 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.8337° |
| argument of perigee: | 275.5929° |
| revolutions per day: | 15.27586469 |
| mean anomaly at epoch: | 84.4770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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