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 18361U 87080A 24280.94138077 .00000314 00000-0 50562-3 0 9996
2 18361 90.3632 63.3996 0104578 22.3188 338.2462 13.44779646817789
| Epoch (UTC): | 06 October 2024 22:35:35 |
| Eccentricity: | 0.0104578 |
| inclination: | 90.3632° |
| perigee height: | 1013 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 63.3996° |
| argument of perigee: | 22.3188° |
| revolutions per day: | 13.44779646 |
| mean anomaly at epoch: | 338.2462° |
| orbit number at epoch: | 81778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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