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 40074U 14037F 23079.14467920 .00007366 00000-0 82145-3 0 9999
2 40074 98.3512 338.9868 0005391 109.7638 250.4117 14.87349609471016
| Epoch (UTC): | 20 March 2023 03:28:20 |
| Eccentricity: | 0.0005391 |
| inclination: | 98.3512° |
| perigee height: | 602 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 338.9868° |
| argument of perigee: | 109.7638° |
| revolutions per day: | 14.87349609 |
| mean anomaly at epoch: | 250.4117° |
| orbit number at epoch: | 47101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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