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 49746C 21115Y 24252.48173611 .00010452 00000+0 65549-3 0 2521
2 49746 53.2159 85.6344 0001193 92.8522 153.3375 15.08826101 19
| Epoch (UTC): | 08 September 2024 11:33:42 |
| Eccentricity: | 0.0001193 |
| inclination: | 53.2159° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 85.6344° |
| argument of perigee: | 92.8522° |
| revolutions per day: | 15.08826101 |
| mean anomaly at epoch: | 153.3375° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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