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 58397U 26075.13395587 +.00000000 +00000-0 +26246-3 0 00009
2 58397 81.2183 328.0869 0029887 320.9868 38.9150 14.16465460 06
| Epoch (UTC): | 16 March 2026 03:12:53 |
| Eccentricity: | 0.0029887 |
| inclination: | 81.2183° |
| perigee height: | 816 km |
| apogee height: | 859 km |
| right ascension of ascending node: | 328.0869° |
| argument of perigee: | 320.9868° |
| revolutions per day: | 14.16465460 |
| mean anomaly at epoch: | 38.9150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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