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 27464U 02036A 23269.91079513 .00000017 00000-0 53700-4 0 9998
2 27464 82.4802 246.6113 0024115 274.3071 85.5254 12.44591558963976
| Epoch (UTC): | 26 September 2023 21:51:32 |
| Eccentricity: | 0.0024115 |
| inclination: | 82.4802° |
| perigee height: | 1468 km |
| apogee height: | 1506 km |
| right ascension of ascending node: | 246.6113° |
| argument of perigee: | 274.3071° |
| revolutions per day: | 12.44591558 |
| mean anomaly at epoch: | 85.5254° |
| orbit number at epoch: | 96397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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