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 58412U 26145.54143736 +.00000000 +00000-0 +39070-3 0 00006
2 58412 42.9967 184.9036 0008875 67.0430 293.1362 15.41644842 03
| Epoch (UTC): | 25 May 2026 12:59:40 |
| Eccentricity: | 0.0008875 |
| inclination: | 42.9967° |
| perigee height: | 435 km |
| apogee height: | 447 km |
| right ascension of ascending node: | 184.9036° |
| argument of perigee: | 67.0430° |
| revolutions per day: | 15.41644842 |
| mean anomaly at epoch: | 293.1362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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