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 34903U 09023A 23253.90162347 0.00000050 00000-0 30131-4 0 00
2 34903 98.9273 351.1746 0008694 343.5401 16.4598 14.06713124 05
| Epoch (UTC): | 10 September 2023 21:38:20 |
| Eccentricity: | 0.0008694 |
| inclination: | 98.9273° |
| perigee height: | 864 km |
| apogee height: | 877 km |
| right ascension of ascending node: | 351.1746° |
| argument of perigee: | 343.5401° |
| revolutions per day: | 14.06713124 |
| mean anomaly at epoch: | 16.4598° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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