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 23332.86569299 .00000329 00000-0 12148-3 0 9997
2 27386 98.2549 296.2976 0001315 84.6784 328.2495 14.38455609139565
| Epoch (UTC): | 28 November 2023 20:46:35 |
| Eccentricity: | 0.0001315 |
| inclination: | 98.2549° |
| perigee height: | 762 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 296.2976° |
| argument of perigee: | 84.6784° |
| revolutions per day: | 14.38455609 |
| mean anomaly at epoch: | 328.2495° |
| orbit number at epoch: | 13956 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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