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 33498U 09002G 23088.52887178 .00005428 00000-0 69882-3 0 9990
2 33498 98.1423 350.1008 0011760 56.0865 304.1463 14.81468802763614
| Epoch (UTC): | 29 March 2023 12:41:34 |
| Eccentricity: | 0.0011760 |
| inclination: | 98.1423° |
| perigee height: | 616 km |
| apogee height: | 633 km |
| right ascension of ascending node: | 350.1008° |
| argument of perigee: | 56.0865° |
| revolutions per day: | 14.81468802 |
| mean anomaly at epoch: | 304.1463° |
| orbit number at epoch: | 76361 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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