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 58090U 26145.32590962 +.00000000 +00000-0 +16663-4 0 00005
2 58090 43.0060 8.7043 0001040 276.1904 83.8829 15.27572530 08
| Epoch (UTC): | 25 May 2026 07:49:18 |
| Eccentricity: | 0.0001040 |
| inclination: | 43.0060° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.7043° |
| argument of perigee: | 276.1904° |
| revolutions per day: | 15.27572530 |
| mean anomaly at epoch: | 83.8829° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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