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 58848U 26145.62881093 +.00000000 +00000-0 +12617-3 0 00001
2 58848 97.3421 205.7674 0012319 88.2180 272.0464 15.15641663 08
| Epoch (UTC): | 25 May 2026 15:05:29 |
| Eccentricity: | 0.0012319 |
| inclination: | 97.3421° |
| perigee height: | 511 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 205.7674° |
| argument of perigee: | 88.2180° |
| revolutions per day: | 15.15641663 |
| mean anomaly at epoch: | 272.0464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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