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 03230U 68040B 24278.52739849 .00012038 00000-0 10206-2 0 9991
2 03230 74.0323 294.6098 0028253 258.0214 101.7805 14.97696759 11826
| Epoch (UTC): | 04 October 2024 12:39:27 |
| Eccentricity: | 0.0028253 |
| inclination: | 74.0323° |
| perigee height: | 554 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 294.6098° |
| argument of perigee: | 258.0214° |
| revolutions per day: | 14.97696759 |
| mean anomaly at epoch: | 101.7805° |
| orbit number at epoch: | 1182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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