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 39430U 13066Q 23087.95493407 .00003954 00000-0 69643-3 0 9998
2 39430 97.7890 343.7570 0145006 226.9350 131.9609 14.61423473497827
| Epoch (UTC): | 28 March 2023 22:55:06 |
| Eccentricity: | 0.0145006 |
| inclination: | 97.7890° |
| perigee height: | 586 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 343.7570° |
| argument of perigee: | 226.9350° |
| revolutions per day: | 14.61423473 |
| mean anomaly at epoch: | 131.9609° |
| orbit number at epoch: | 49782 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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