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 22183.57520630 .00001034 00000-0 12695-3 0 9998
2 40074 98.3814 65.0365 0003050 238.6004 121.4916 14.85445002432316
| Epoch (UTC): | 02 July 2022 13:48:17 |
| Eccentricity: | 0.0003050 |
| inclination: | 98.3814° |
| perigee height: | 610 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 65.0365° |
| argument of perigee: | 238.6004° |
| revolutions per day: | 14.85445002 |
| mean anomaly at epoch: | 121.4916° |
| orbit number at epoch: | 43231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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