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 18422U 87088B 23150.45116813 .00000503 00000-0 57974-4 0 9992
2 18422 82.5100 299.9367 0020736 117.5949 242.7376 14.83578148902847
| Epoch (UTC): | 30 May 2023 10:49:40 |
| Eccentricity: | 0.0020736 |
| inclination: | 82.5100° |
| perigee height: | 603 km |
| apogee height: | 632 km |
| right ascension of ascending node: | 299.9367° |
| argument of perigee: | 117.5949° |
| revolutions per day: | 14.83578148 |
| mean anomaly at epoch: | 242.7376° |
| orbit number at epoch: | 90284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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