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 18421U 87088A 23150.42438702 .00006811 00000-0 27523-3 0 9996
2 18421 82.4956 284.5995 0011625 273.7804 86.2104 15.24515191948039
| Epoch (UTC): | 30 May 2023 10:11:07 |
| Eccentricity: | 0.0011625 |
| inclination: | 82.4956° |
| perigee height: | 484 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 284.5995° |
| argument of perigee: | 273.7804° |
| revolutions per day: | 15.24515191 |
| mean anomaly at epoch: | 86.2104° |
| orbit number at epoch: | 94803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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