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 33493U 09002B 23335.01077797 .00019054 00000-0 11395-2 0 9997
2 33493 98.2338 1.6738 0013868 199.8419 160.2271 15.11032186808901
| Epoch (UTC): | 01 December 2023 00:15:31 |
| Eccentricity: | 0.0013868 |
| inclination: | 98.2338° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 1.6738° |
| argument of perigee: | 199.8419° |
| revolutions per day: | 15.11032186 |
| mean anomaly at epoch: | 160.2271° |
| orbit number at epoch: | 80890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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