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 33505U 09003B 23337.29775812 .00004089 00000-0 23043-3 0 9993
2 33505 82.3888 55.0604 0023399 357.9212 2.1917 15.12706324817018
| Epoch (UTC): | 03 December 2023 07:08:46 |
| Eccentricity: | 0.0023399 |
| inclination: | 82.3888° |
| perigee height: | 512 km |
| apogee height: | 544 km |
| right ascension of ascending node: | 55.0604° |
| argument of perigee: | 357.9212° |
| revolutions per day: | 15.12706324 |
| mean anomaly at epoch: | 2.1917° |
| orbit number at epoch: | 81701 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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