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 42468U 10057BH 24214.23345873 .00000552 00000-0 48231-2 0 9997
2 42468 20.3836 273.0152 7191679 201.2915 98.5651 2.26201465 79084
| Epoch (UTC): | 01 August 2024 05:36:10 |
| Eccentricity: | 0.7191679 |
| inclination: | 20.3836° |
| perigee height: | 506 km |
| apogee height: | 35764 km |
| right ascension of ascending node: | 273.0152° |
| argument of perigee: | 201.2915° |
| revolutions per day: | 2.26201465 |
| mean anomaly at epoch: | 98.5651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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