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 23080.28834429 .00007000 00000-0 78078-3 0 9993
2 40074 98.3517 340.1901 0005304 106.3112 253.8665 14.87362661471184
| Epoch (UTC): | 21 March 2023 06:55:12 |
| Eccentricity: | 0.0005304 |
| inclination: | 98.3517° |
| perigee height: | 602 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 340.1901° |
| argument of perigee: | 106.3112° |
| revolutions per day: | 14.87362661 |
| mean anomaly at epoch: | 253.8665° |
| orbit number at epoch: | 47118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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