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 58363U 26145.42823941 +.00000000 +00000-0 +27084-3 0 00003
2 58363 43.0047 277.2228 0002698 274.8813 85.1730 15.27603921 03
| Epoch (UTC): | 25 May 2026 10:16:39 |
| Eccentricity: | 0.0002698 |
| inclination: | 43.0047° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 277.2228° |
| argument of perigee: | 274.8813° |
| revolutions per day: | 15.27603921 |
| mean anomaly at epoch: | 85.1730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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