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 40376U 15003A 23150.43848085 .00000508 00000-0 10735-3 0 9992
2 40376 98.1273 157.2600 0001298 88.6366 271.4985 14.63377979444734
| Epoch (UTC): | 30 May 2023 10:31:24 |
| Eccentricity: | 0.0001298 |
| inclination: | 98.1273° |
| perigee height: | 681 km |
| apogee height: | 683 km |
| right ascension of ascending node: | 157.2600° |
| argument of perigee: | 88.6366° |
| revolutions per day: | 14.63377979 |
| mean anomaly at epoch: | 271.4985° |
| orbit number at epoch: | 44473 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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