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 58437U 26145.52066654 +.00000000 +00000-0 +10539-3 0 00003
2 58437 42.9999 327.8062 0002113 275.9983 84.0628 15.27577893 01
| Epoch (UTC): | 25 May 2026 12:29:45 |
| Eccentricity: | 0.0002113 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 327.8062° |
| argument of perigee: | 275.9983° |
| revolutions per day: | 15.27577893 |
| mean anomaly at epoch: | 84.0628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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