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 24278U 96046B 23088.48040238 .00000044 00000-0 83760-4 0 9994
2 24278 98.5234 77.9182 0349185 263.6536 92.4735 13.53139903314152
| Epoch (UTC): | 29 March 2023 11:31:46 |
| Eccentricity: | 0.0349185 |
| inclination: | 98.5234° |
| perigee height: | 801 km |
| apogee height: | 1320 km |
| right ascension of ascending node: | 77.9182° |
| argument of perigee: | 263.6536° |
| revolutions per day: | 13.53139903 |
| mean anomaly at epoch: | 92.4735° |
| orbit number at epoch: | 31415 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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