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 40299U 14070B 23088.87526910 .00015084 00000-0 49376-3 0 9995
2 40299 97.2025 153.6715 0011053 193.1297 283.6483 15.31711850466665
| Epoch (UTC): | 29 March 2023 21:00:23 |
| Eccentricity: | 0.0011053 |
| inclination: | 97.2025° |
| perigee height: | 463 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 153.6715° |
| argument of perigee: | 193.1297° |
| revolutions per day: | 15.31711850 |
| mean anomaly at epoch: | 283.6483° |
| orbit number at epoch: | 46666 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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