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 58172U 26145.53920160 +.00000000 +00000-0 -38897-5 0 00001
2 58172 67.1514 342.4745 0016113 327.5284 32.4808 13.97332366 09
| Epoch (UTC): | 25 May 2026 12:56:27 |
| Eccentricity: | 0.0016113 |
| inclination: | 67.1514° |
| perigee height: | 891 km |
| apogee height: | 915 km |
| right ascension of ascending node: | 342.4745° |
| argument of perigee: | 327.5284° |
| revolutions per day: | 13.97332366 |
| mean anomaly at epoch: | 32.4808° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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