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 58803U 26145.19115962 +.00000000 +00000-0 +10333-3 0 00002
2 58803 43.0026 93.3940 0001565 266.6808 93.3865 15.27594741 01
| Epoch (UTC): | 25 May 2026 04:35:16 |
| Eccentricity: | 0.0001565 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.3940° |
| argument of perigee: | 266.6808° |
| revolutions per day: | 15.27594741 |
| mean anomaly at epoch: | 93.3865° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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