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 58218U 26145.39513336 +.00000000 +00000-0 +84494-4 0 00001
2 58218 43.0025 120.7533 0001741 263.8288 96.2365 15.27575172 04
| Epoch (UTC): | 25 May 2026 09:28:59 |
| Eccentricity: | 0.0001741 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 120.7533° |
| argument of perigee: | 263.8288° |
| revolutions per day: | 15.27575172 |
| mean anomaly at epoch: | 96.2365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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