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 40554U 15020C 23273.51483910 .00000022 00000-0 88028-4 0 9998
2 40554 82.4803 288.0021 0012912 340.0680 19.9894 12.42897027385718
| Epoch (UTC): | 30 September 2023 12:21:22 |
| Eccentricity: | 0.0012912 |
| inclination: | 82.4803° |
| perigee height: | 1484 km |
| apogee height: | 1504 km |
| right ascension of ascending node: | 288.0021° |
| argument of perigee: | 340.0680° |
| revolutions per day: | 12.42897027 |
| mean anomaly at epoch: | 19.9894° |
| orbit number at epoch: | 38571 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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