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 38773U 12048P 22329.81258302 0.00000000 00000-0 00000-0 0 03
2 38773 63.4435 281.4335 0201859 359.1479 0.8521 13.40847803 08
| Epoch (UTC): | 25 November 2022 19:30:07 |
| Eccentricity: | 0.0201859 |
| inclination: | 63.4435° |
| perigee height: | 955 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 281.4335° |
| argument of perigee: | 359.1479° |
| revolutions per day: | 13.40847803 |
| mean anomaly at epoch: | 0.8521° |
| 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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