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 40025U 14033R 23086.79876199 .00008174 00000-0 79150-3 0 9992
2 40025 97.9897 32.1980 0010652 193.2047 166.8895 14.92959838475990
| Epoch (UTC): | 27 March 2023 19:10:13 |
| Eccentricity: | 0.0010652 |
| inclination: | 97.9897° |
| perigee height: | 581 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 32.1980° |
| argument of perigee: | 193.2047° |
| revolutions per day: | 14.92959838 |
| mean anomaly at epoch: | 166.8895° |
| orbit number at epoch: | 47599 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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