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 18986U 88023B 23086.04811162 .00000221 00000-0 20123-3 0 9991
2 18986 82.9497 274.5300 0042777 58.2296 302.3019 13.78717366761206
| Epoch (UTC): | 27 March 2023 01:09:16 |
| Eccentricity: | 0.0042777 |
| inclination: | 82.9497° |
| perigee height: | 937 km |
| apogee height: | 1000 km |
| right ascension of ascending node: | 274.5300° |
| argument of perigee: | 58.2296° |
| revolutions per day: | 13.78717366 |
| mean anomaly at epoch: | 302.3019° |
| orbit number at epoch: | 76120 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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