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 18362U 87080B 24251.93908375 .00000314 00000-0 50670-3 0 9990
2 18362 90.3601 62.7711 0107266 125.8631 349.3313 13.44327209813185
| Epoch (UTC): | 07 September 2024 22:32:16 |
| Eccentricity: | 0.0107266 |
| inclination: | 90.3601° |
| perigee height: | 1013 km |
| apogee height: | 1173 km |
| right ascension of ascending node: | 62.7711° |
| argument of perigee: | 125.8631° |
| revolutions per day: | 13.44327209 |
| mean anomaly at epoch: | 349.3313° |
| orbit number at epoch: | 81318 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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