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 47478U 21006BT 24251.74123796 .00096737 00000-0 13472-2 0 9993
2 47478 97.3180 317.1629 0004324 248.8658 111.2135 15.56604017201746
| Epoch (UTC): | 07 September 2024 17:47:22 |
| Eccentricity: | 0.0004324 |
| inclination: | 97.3180° |
| perigee height: | 394 km |
| apogee height: | 400 km |
| right ascension of ascending node: | 317.1629° |
| argument of perigee: | 248.8658° |
| revolutions per day: | 15.56604017 |
| mean anomaly at epoch: | 111.2135° |
| orbit number at epoch: | 20174 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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