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 23150.51888334 -.00000004 00000-0 28666-4 0 9996
2 24278 98.5274 131.4837 0351271 102.6822 261.3823 13.53145120322543
| Epoch (UTC): | 30 May 2023 12:27:11 |
| Eccentricity: | 0.0351271 |
| inclination: | 98.5274° |
| perigee height: | 799 km |
| apogee height: | 1322 km |
| right ascension of ascending node: | 131.4837° |
| argument of perigee: | 102.6822° |
| revolutions per day: | 13.53145120 |
| mean anomaly at epoch: | 261.3823° |
| orbit number at epoch: | 32254 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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