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 23085.99859546 .00044778 00000-0 12147-2 0 9995
2 40912 97.4262 102.5103 0010408 33.6666 20.6880 15.37430413416953
| Epoch (UTC): | 26 March 2023 23:57:58 |
| Eccentricity: | 0.0010408 |
| inclination: | 97.4262° |
| perigee height: | 446 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 102.5103° |
| argument of perigee: | 33.6666° |
| revolutions per day: | 15.37430413 |
| mean anomaly at epoch: | 20.6880° |
| orbit number at epoch: | 41695 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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