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 40378U 15003C 23088.87340399 .00111340 00000-0 16464-2 0 9998
2 40378 99.0781 25.8846 0065721 124.9375 235.8070 15.52396788452261
| Epoch (UTC): | 29 March 2023 20:57:42 |
| Eccentricity: | 0.0065721 |
| inclination: | 99.0781° |
| perigee height: | 365 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 25.8846° |
| argument of perigee: | 124.9375° |
| revolutions per day: | 15.52396788 |
| mean anomaly at epoch: | 235.8070° |
| orbit number at epoch: | 45226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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