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 58890U 26145.46430943 +.00000000 +00000-0 +50289-4 0 00002
2 58890 53.1614 323.1411 0000937 97.0867 263.0242 15.34392622 09
| Epoch (UTC): | 25 May 2026 11:08:36 |
| Eccentricity: | 0.0000937 |
| inclination: | 53.1614° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 323.1411° |
| argument of perigee: | 97.0867° |
| revolutions per day: | 15.34392622 |
| mean anomaly at epoch: | 263.0242° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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