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 49122U 21079A 24282.87051888 .00002153 00000-0 48114-3 0 9992
2 49122 98.1692 356.0567 0002476 60.6545 299.4901 14.57750634164290
| Epoch (UTC): | 08 October 2024 20:53:32 |
| Eccentricity: | 0.0002476 |
| inclination: | 98.1692° |
| perigee height: | 698 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 356.0567° |
| argument of perigee: | 60.6545° |
| revolutions per day: | 14.57750634 |
| mean anomaly at epoch: | 299.4901° |
| orbit number at epoch: | 16429 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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