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 24297U 96051A 23266.46648382 -.00000092 00000-0 -22986-4 0 9999
2 24297 70.9040 275.7003 0024020 3.0948 357.0317 14.13492508395293
| Epoch (UTC): | 23 September 2023 11:11:44 |
| Eccentricity: | 0.0024020 |
| inclination: | 70.9040° |
| perigee height: | 830 km |
| apogee height: | 865 km |
| right ascension of ascending node: | 275.7003° |
| argument of perigee: | 3.0948° |
| revolutions per day: | 14.13492508 |
| mean anomaly at epoch: | 357.0317° |
| orbit number at epoch: | 39529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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