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 58095U 26145.30454759 +.00000000 +00000-0 +45105-5 0 00005
2 58095 43.0053 5.1504 0001428 269.7242 90.3446 15.27577730 06
| Epoch (UTC): | 25 May 2026 07:18:32 |
| Eccentricity: | 0.0001428 |
| inclination: | 43.0053° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 5.1504° |
| argument of perigee: | 269.7242° |
| revolutions per day: | 15.27577730 |
| mean anomaly at epoch: | 90.3446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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