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 24251.72245710 .00014337 00000-0 16119-2 0 9998
2 33498 98.1131 167.6235 0011438 130.9471 229.2735 14.86769226841930
| Epoch (UTC): | 07 September 2024 17:20:20 |
| Eccentricity: | 0.0011438 |
| inclination: | 98.1131° |
| perigee height: | 600 km |
| apogee height: | 616 km |
| right ascension of ascending node: | 167.6235° |
| argument of perigee: | 130.9471° |
| revolutions per day: | 14.86769226 |
| mean anomaly at epoch: | 229.2735° |
| orbit number at epoch: | 84193 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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