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 23268.94088079 .00020407 00000-0 12953-2 0 9994
2 33493 98.2435 290.6804 0016944 71.2545 289.0518 15.08802728798921
| Epoch (UTC): | 25 September 2023 22:34:52 |
| Eccentricity: | 0.0016944 |
| inclination: | 98.2435° |
| perigee height: | 528 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 290.6804° |
| argument of perigee: | 71.2545° |
| revolutions per day: | 15.08802728 |
| mean anomaly at epoch: | 289.0518° |
| orbit number at epoch: | 79892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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