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 23151.86838235 .00007736 00000-0 31253-3 0 9992
2 18421 82.4957 283.1528 0011607 268.2417 91.7491 15.24537333948252
| Epoch (UTC): | 31 May 2023 20:50:28 |
| Eccentricity: | 0.0011607 |
| inclination: | 82.4957° |
| perigee height: | 484 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 283.1528° |
| argument of perigee: | 268.2417° |
| revolutions per day: | 15.24537333 |
| mean anomaly at epoch: | 91.7491° |
| orbit number at epoch: | 94825 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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