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 23266.69702118 .00004541 00000-0 56959-3 0 9992
2 33498 98.1242 171.1377 0009680 186.5100 173.5988 14.82660129790428
| Epoch (UTC): | 23 September 2023 16:43:42 |
| Eccentricity: | 0.0009680 |
| inclination: | 98.1242° |
| perigee height: | 614 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 171.1377° |
| argument of perigee: | 186.5100° |
| revolutions per day: | 14.82660129 |
| mean anomaly at epoch: | 173.5988° |
| orbit number at epoch: | 79042 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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