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 23078.82271975 .00006164 00000-0 60064-3 0 9999
2 40025 97.9884 24.1014 0009886 223.8266 136.2169 14.92819143474803
| Epoch (UTC): | 19 March 2023 19:44:42 |
| Eccentricity: | 0.0009886 |
| inclination: | 97.9884° |
| perigee height: | 582 km |
| apogee height: | 596 km |
| right ascension of ascending node: | 24.1014° |
| argument of perigee: | 223.8266° |
| revolutions per day: | 14.92819143 |
| mean anomaly at epoch: | 136.2169° |
| orbit number at epoch: | 47480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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