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 58231U 26145.22740245 +.00000000 +00000-0 +36770-4 0 00003
2 58231 43.0044 212.6784 0001484 272.7861 87.2820 15.27570070 07
| Epoch (UTC): | 25 May 2026 05:27:27 |
| Eccentricity: | 0.0001484 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 212.6784° |
| argument of perigee: | 272.7861° |
| revolutions per day: | 15.27570070 |
| mean anomaly at epoch: | 87.2820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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