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 23157.46937189 -.00000008 00000-0 24300-4 0 9995
2 24278 98.5277 137.4857 0351339 84.7099 279.4020 13.53145504323484
| Epoch (UTC): | 06 June 2023 11:15:53 |
| Eccentricity: | 0.0351339 |
| inclination: | 98.5277° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 137.4857° |
| argument of perigee: | 84.7099° |
| revolutions per day: | 13.53145504 |
| mean anomaly at epoch: | 279.4020° |
| orbit number at epoch: | 32348 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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