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 58023U 26145.46351536 +.00000000 +00000-0 +21468-3 0 00006
2 58023 97.5691 226.8540 0003363 103.7066 256.4545 15.23589891 04
| Epoch (UTC): | 25 May 2026 11:07:27 |
| Eccentricity: | 0.0003363 |
| inclination: | 97.5691° |
| perigee height: | 493 km |
| apogee height: | 497 km |
| right ascension of ascending node: | 226.8540° |
| argument of perigee: | 103.7066° |
| revolutions per day: | 15.23589891 |
| mean anomaly at epoch: | 256.4545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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