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 27386U 02009A 23270.88758205 .00000270 00000-0 10208-3 0 9997
2 27386 98.2436 236.7320 0001215 88.0311 325.8845 14.38412801130723
| Epoch (UTC): | 27 September 2023 21:18:07 |
| Eccentricity: | 0.0001215 |
| inclination: | 98.2436° |
| perigee height: | 763 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 236.7320° |
| argument of perigee: | 88.0311° |
| revolutions per day: | 14.38412801 |
| mean anomaly at epoch: | 325.8845° |
| orbit number at epoch: | 13072 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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