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 23081.29745556 .00006181 00000-0 69018-3 0 9990
2 40074 98.3513 341.2507 0005340 101.5922 258.5872 14.87369953471330
| Epoch (UTC): | 22 March 2023 07:08:20 |
| Eccentricity: | 0.0005340 |
| inclination: | 98.3513° |
| perigee height: | 602 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 341.2507° |
| argument of perigee: | 101.5922° |
| revolutions per day: | 14.87369953 |
| mean anomaly at epoch: | 258.5872° |
| orbit number at epoch: | 47133 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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