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 39232U 13043A 22280.83608290 0.00035000 00000-0 37217-3 0 04
2 39232 97.9270 342.5504 0542590 172.6129 187.4380 14.73994334 09
| Epoch (UTC): | 07 October 2022 20:03:57 |
| Eccentricity: | 0.0542590 |
| inclination: | 97.9270° |
| perigee height: | 267 km |
| apogee height: | 1029 km |
| right ascension of ascending node: | 342.5504° |
| argument of perigee: | 172.6129° |
| revolutions per day: | 14.73994334 |
| mean anomaly at epoch: | 187.4380° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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