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 43223U 18021A 24244.92288824 0.00000000 00000-0 00000-0 0 08
2 43223 97.3489 3.2599 0004327 51.9105 308.0481 15.27646025 03
| Epoch (UTC): | 31 August 2024 22:08:57 |
| Eccentricity: | 0.0004327 |
| inclination: | 97.3489° |
| perigee height: | 480 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 3.2599° |
| argument of perigee: | 51.9105° |
| revolutions per day: | 15.27646025 |
| mean anomaly at epoch: | 308.0481° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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