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 40380U 15003E 23334.84698270 .00061897 00000-0 11614-2 0 9999
2 40380 99.0972 300.7392 0078433 92.9209 268.1014 15.45028221488342
| Epoch (UTC): | 30 November 2023 20:19:39 |
| Eccentricity: | 0.0078433 |
| inclination: | 99.0972° |
| perigee height: | 378 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 300.7392° |
| argument of perigee: | 92.9209° |
| revolutions per day: | 15.45028221 |
| mean anomaly at epoch: | 268.1014° |
| orbit number at epoch: | 48834 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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