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 62024U 26145.48223311 +.00000000 +00000-0 +43415-3 0 00009
2 62024 53.1591 171.3269 0000955 78.9633 281.1475 15.30210789 08
| Epoch (UTC): | 25 May 2026 11:34:24 |
| Eccentricity: | 0.0000955 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 171.3269° |
| argument of perigee: | 78.9633° |
| revolutions per day: | 15.30210789 |
| mean anomaly at epoch: | 281.1475° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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