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 42785U 17036W 24093.93150985 .15183516 24061-5 25581-3 0 9993
2 42785 97.0682 134.7147 0009955 258.1285 101.8903 16.47509988378182
| Epoch (UTC): | 02 April 2024 22:21:22 |
| Eccentricity: | 0.0009955 |
| inclination: | 97.0682° |
| perigee height: | 139 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 134.7147° |
| argument of perigee: | 258.1285° |
| revolutions per day: | 16.47509988 |
| mean anomaly at epoch: | 101.8903° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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