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 58893U 26145.46486884 +.00000000 +00000-0 +45273-4 0 00007
2 58893 53.1606 325.2449 0001089 98.7152 261.3974 15.34391614 04
| Epoch (UTC): | 25 May 2026 11:09:24 |
| Eccentricity: | 0.0001089 |
| inclination: | 53.1606° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 325.2449° |
| argument of perigee: | 98.7152° |
| revolutions per day: | 15.34391614 |
| mean anomaly at epoch: | 261.3974° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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