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 38483U 93036BTT 24252.34963700 .00009797 00000-0 39139-2 0 9993
2 38483 74.2638 113.5252 0118484 356.1855 3.8376 14.24751185776843
| Epoch (UTC): | 08 September 2024 08:23:28 |
| Eccentricity: | 0.0118484 |
| inclination: | 74.2638° |
| perigee height: | 724 km |
| apogee height: | 894 km |
| right ascension of ascending node: | 113.5252° |
| argument of perigee: | 356.1855° |
| revolutions per day: | 14.24751185 |
| mean anomaly at epoch: | 3.8376° |
| orbit number at epoch: | 77684 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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