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 40302U 14070E 23274.12374011 .00030760 00000-0 93373-3 0 9992
2 40302 97.1230 282.5138 0026094 348.1205 11.9419 15.33694084493189
| Epoch (UTC): | 01 October 2023 02:58:11 |
| Eccentricity: | 0.0026094 |
| inclination: | 97.1230° |
| perigee height: | 447 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 282.5138° |
| argument of perigee: | 348.1205° |
| revolutions per day: | 15.33694084 |
| mean anomaly at epoch: | 11.9419° |
| orbit number at epoch: | 49318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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