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 58555U 26145.61398056 +.00000000 +00000-0 +79609-2 0 00000
2 58555 97.2793 136.4743 0040670 355.6856 4.4025 15.23550637 02
| Epoch (UTC): | 25 May 2026 14:44:07 |
| Eccentricity: | 0.0040670 |
| inclination: | 97.2793° |
| perigee height: | 467 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 136.4743° |
| argument of perigee: | 355.6856° |
| revolutions per day: | 15.23550637 |
| mean anomaly at epoch: | 4.4025° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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