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 40448U 95015BA 24278.41460171 .00020507 00000-0 98377-2 0 9997
2 40448 98.9481 262.6981 0043614 32.8298 327.5573 14.18411965493227
| Epoch (UTC): | 04 October 2024 09:57:01 |
| Eccentricity: | 0.0043614 |
| inclination: | 98.9481° |
| perigee height: | 799 km |
| apogee height: | 862 km |
| right ascension of ascending node: | 262.6981° |
| argument of perigee: | 32.8298° |
| revolutions per day: | 14.18411965 |
| mean anomaly at epoch: | 327.5573° |
| orbit number at epoch: | 49322 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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