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 29948U 99025JW 24358.20185312 .00000362 00000-0 23909-3 0 9998
2 29948 98.7953 347.9500 0085261 148.7188 340.3936 14.05924582920089
| Epoch (UTC): | 23 December 2024 04:50:40 |
| Eccentricity: | 0.0085261 |
| inclination: | 98.7953° |
| perigee height: | 811 km |
| apogee height: | 935 km |
| right ascension of ascending node: | 347.9500° |
| argument of perigee: | 148.7188° |
| revolutions per day: | 14.05924582 |
| mean anomaly at epoch: | 340.3936° |
| orbit number at epoch: | 92008 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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