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 23156.80054247 .00002620 00000-0 33722-3 0 9995
2 33498 98.1373 59.4733 0010013 182.4372 177.6793 14.81963421774145
| Epoch (UTC): | 05 June 2023 19:12:46 |
| Eccentricity: | 0.0010013 |
| inclination: | 98.1373° |
| perigee height: | 616 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 59.4733° |
| argument of perigee: | 182.4372° |
| revolutions per day: | 14.81963421 |
| mean anomaly at epoch: | 177.6793° |
| orbit number at epoch: | 77414 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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