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 09988U 74089EF 24357.84766030 .00002156 00000-0 14032-2 0 9993
2 09988 103.0447 195.3526 0237644 58.4908 303.9217 13.91383303429044
| Epoch (UTC): | 22 December 2024 20:20:37 |
| Eccentricity: | 0.0237644 |
| inclination: | 103.0447° |
| perigee height: | 750 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 195.3526° |
| argument of perigee: | 58.4908° |
| revolutions per day: | 13.91383303 |
| mean anomaly at epoch: | 303.9217° |
| orbit number at epoch: | 42904 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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