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 23331.72808941 .00008428 00000-0 87196-3 0 9997
2 40074 98.3390 244.9126 0005113 34.8529 325.3021 14.90348069508595
| Epoch (UTC): | 27 November 2023 17:28:26 |
| Eccentricity: | 0.0005113 |
| inclination: | 98.3390° |
| perigee height: | 593 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 244.9126° |
| argument of perigee: | 34.8529° |
| revolutions per day: | 14.90348069 |
| mean anomaly at epoch: | 325.3021° |
| orbit number at epoch: | 50859 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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