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 10703U 78026B 23266.85424062 .00000488 00000-0 36660-3 0 9998
2 10703 99.2165 233.6299 0007378 131.2861 288.3027 13.99428302324804
| Epoch (UTC): | 23 September 2023 20:30:06 |
| Eccentricity: | 0.0007378 |
| inclination: | 99.2165° |
| perigee height: | 890 km |
| apogee height: | 901 km |
| right ascension of ascending node: | 233.6299° |
| argument of perigee: | 131.2861° |
| revolutions per day: | 13.99428302 |
| mean anomaly at epoch: | 288.3027° |
| orbit number at epoch: | 32480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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