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 18152U 87055A 24263.38835348 .00012379 00000-0 59841-3 0 9993
2 18152 82.4901 225.7637 0014209 99.8813 260.4026 15.18416296 8088
| Epoch (UTC): | 19 September 2024 09:19:13 |
| Eccentricity: | 0.0014209 |
| inclination: | 82.4901° |
| perigee height: | 501 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 225.7637° |
| argument of perigee: | 99.8813° |
| revolutions per day: | 15.18416296 |
| mean anomaly at epoch: | 260.4026° |
| orbit number at epoch: | 808 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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