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 43678U 18084H 23087.57833717 .00003453 00000-0 33678-3 0 9995
2 43678 98.0074 230.0021 0010807 70.3666 289.8677 14.93093940240230
| Epoch (UTC): | 28 March 2023 13:52:48 |
| Eccentricity: | 0.0010807 |
| inclination: | 98.0074° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 230.0021° |
| argument of perigee: | 70.3666° |
| revolutions per day: | 14.93093940 |
| mean anomaly at epoch: | 289.8677° |
| orbit number at epoch: | 24023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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