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 55080U 23001BZ 23266.41669438 .00011352 00000-0 52690-3 0 9991
2 55080 97.4671 325.2820 0014944 32.2662 327.9484 15.20094425 40002
| Epoch (UTC): | 23 September 2023 10:00:02 |
| Eccentricity: | 0.0014944 |
| inclination: | 97.4671° |
| perigee height: | 495 km |
| apogee height: | 516 km |
| right ascension of ascending node: | 325.2820° |
| argument of perigee: | 32.2662° |
| revolutions per day: | 15.20094425 |
| mean anomaly at epoch: | 327.9484° |
| orbit number at epoch: | 4000 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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