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 data is extracted from the following two-line orbital elements,
1 23088U 94023B 24284.14180244 .00000119 00000-0 86101-4 0 9994
2 23088 70.9995 73.4988 0004268 324.8136 35.2705 14.14895552573436
| Epoch (UTC): | 10 October 2024 03:24:11 |
| Eccentricity: | 0.0004268 |
| inclination: | 70.9995° |
| perigee height: | 839 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 73.4988° |
| argument of perigee: | 324.8136° |
| revolutions per day: | 14.14895552 |
| mean anomaly at epoch: | 35.2705° |
| orbit number at epoch: | 57343 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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