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 40381U 15004A 23075.84473526 0.00000000 00000-0 00000-0 0 05
2 40381 97.3521 148.3463 0001893 62.7454 297.2544 15.27650051 08
| Epoch (UTC): | 16 March 2023 20:16:25 |
| Eccentricity: | 0.0001893 |
| inclination: | 97.3521° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 148.3463° |
| argument of perigee: | 62.7454° |
| revolutions per day: | 15.27650051 |
| mean anomaly at epoch: | 297.2544° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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