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 58443U 26145.54251161 +.00000000 +00000-0 +16808-3 0 00006
2 58443 43.0012 327.9627 0001445 262.8945 97.1742 15.27574613 03
| Epoch (UTC): | 25 May 2026 13:01:13 |
| Eccentricity: | 0.0001445 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9627° |
| argument of perigee: | 262.8945° |
| revolutions per day: | 15.27574613 |
| mean anomaly at epoch: | 97.1742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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