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 24954U 97052B 23081.54421617 .00000130 00000-0 10947-3 0 9999
2 24954 82.9242 150.5656 0040277 40.5951 77.4231 13.80099613283855
| Epoch (UTC): | 22 March 2023 13:03:40 |
| Eccentricity: | 0.0040277 |
| inclination: | 82.9242° |
| perigee height: | 934 km |
| apogee height: | 993 km |
| right ascension of ascending node: | 150.5656° |
| argument of perigee: | 40.5951° |
| revolutions per day: | 13.80099613 |
| mean anomaly at epoch: | 77.4231° |
| orbit number at epoch: | 28385 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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