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 23851U 96024A 23088.43604973 .00000019 00000-0 43526-4 0 9991
2 23851 98.9230 33.9709 0006673 235.8404 124.2127 13.98164685374038
| Epoch (UTC): | 29 March 2023 10:27:54 |
| Eccentricity: | 0.0006673 |
| inclination: | 98.9230° |
| perigee height: | 895 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 33.9709° |
| argument of perigee: | 235.8404° |
| revolutions per day: | 13.98164685 |
| mean anomaly at epoch: | 124.2127° |
| orbit number at epoch: | 37403 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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