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 55049U 23001AS 23267.09675194 .00013288 00000-0 64627-3 0 9990
2 55049 97.4699 325.3756 0012794 32.5274 327.6745 15.18460380 40066
| Epoch (UTC): | 24 September 2023 02:19:19 |
| Eccentricity: | 0.0012794 |
| inclination: | 97.4699° |
| perigee height: | 501 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 325.3756° |
| argument of perigee: | 32.5274° |
| revolutions per day: | 15.18460380 |
| mean anomaly at epoch: | 327.6745° |
| orbit number at epoch: | 4006 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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