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 40912U 15049P 23080.33611322 .00039445 00000-0 10900-2 0 9996
2 40912 97.4266 96.7890 0011570 50.9381 8.9866 15.36872954416087
| Epoch (UTC): | 21 March 2023 08:04:00 |
| Eccentricity: | 0.0011570 |
| inclination: | 97.4266° |
| perigee height: | 447 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 96.7890° |
| argument of perigee: | 50.9381° |
| revolutions per day: | 15.36872954 |
| mean anomaly at epoch: | 8.9866° |
| orbit number at epoch: | 41608 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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