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 58971U 26145.39467409 +.00000000 +00000-0 +40618-4 0 00006
2 58971 53.1609 287.8652 0001259 86.0581 274.0564 15.30194862 06
| Epoch (UTC): | 25 May 2026 09:28:19 |
| Eccentricity: | 0.0001259 |
| inclination: | 53.1609° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.8652° |
| argument of perigee: | 86.0581° |
| revolutions per day: | 15.30194862 |
| mean anomaly at epoch: | 274.0564° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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