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 58840U 26145.38637007 +.00000000 +00000-0 +43682-4 0 00007
2 58840 53.1607 219.7798 0000753 98.7335 261.3753 15.34389369 00
| Epoch (UTC): | 25 May 2026 09:16:22 |
| Eccentricity: | 0.0000753 |
| inclination: | 53.1607° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 219.7798° |
| argument of perigee: | 98.7335° |
| revolutions per day: | 15.34389369 |
| mean anomaly at epoch: | 261.3753° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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