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 58628U 26145.59182803 +.00000000 +00000-0 +11760-3 0 00004
2 58628 43.0020 352.6994 0001475 275.7262 84.3422 15.27580162 06
| Epoch (UTC): | 25 May 2026 14:12:13 |
| Eccentricity: | 0.0001475 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 352.6994° |
| argument of perigee: | 275.7262° |
| revolutions per day: | 15.27580162 |
| mean anomaly at epoch: | 84.3422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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