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 40912U 15049P 23158.74143826 .00035940 00000-0 80731-3 0 9992
2 40912 97.4166 176.3412 0011390 115.4947 244.7480 15.43208454428155
| Epoch (UTC): | 07 June 2023 17:47:40 |
| Eccentricity: | 0.0011390 |
| inclination: | 97.4166° |
| perigee height: | 429 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 176.3412° |
| argument of perigee: | 115.4947° |
| revolutions per day: | 15.43208454 |
| mean anomaly at epoch: | 244.7480° |
| orbit number at epoch: | 42815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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