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 58542U 26145.48503008 +.00000000 +00000-0 +37799-4 0 00002
2 58542 53.1608 65.2858 0001315 94.8225 265.2928 15.34389736 06
| Epoch (UTC): | 25 May 2026 11:38:26 |
| Eccentricity: | 0.0001315 |
| inclination: | 53.1608° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 65.2858° |
| argument of perigee: | 94.8225° |
| revolutions per day: | 15.34389736 |
| mean anomaly at epoch: | 265.2928° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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