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 41338U 16012B 23083.17241831 .00020095 00000-0 14387-2 0 9993
2 41338 31.0040 41.0412 0012036 49.6655 310.5031 15.03236705389575
| Epoch (UTC): | 24 March 2023 04:08:16 |
| Eccentricity: | 0.0012036 |
| inclination: | 31.0040° |
| perigee height: | 548 km |
| apogee height: | 565 km |
| right ascension of ascending node: | 41.0412° |
| argument of perigee: | 49.6655° |
| revolutions per day: | 15.03236705 |
| mean anomaly at epoch: | 310.5031° |
| orbit number at epoch: | 38957 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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