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 40034U 14033AA 23033.45710999 .00003127 00000-0 44775-3 0 9990
2 40034 97.6612 215.5720 0057373 130.4191 230.2045 14.76134250463372
| Epoch (UTC): | 02 February 2023 10:58:14 |
| Eccentricity: | 0.0057373 |
| inclination: | 97.6612° |
| perigee height: | 601 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 215.5720° |
| argument of perigee: | 130.4191° |
| revolutions per day: | 14.76134250 |
| mean anomaly at epoch: | 230.2045° |
| orbit number at epoch: | 46337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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