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 39440U 13066AA 23334.47432915 .00006618 00000-0 82277-3 0 9996
2 39440 97.7926 278.1041 0072144 204.7367 155.0380 14.81025776539956
| Epoch (UTC): | 30 November 2023 11:23:02 |
| Eccentricity: | 0.0072144 |
| inclination: | 97.7926° |
| perigee height: | 575 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 278.1041° |
| argument of perigee: | 204.7367° |
| revolutions per day: | 14.81025776 |
| mean anomaly at epoch: | 155.0380° |
| orbit number at epoch: | 53995 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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