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 11378U 79046A 23033.56278878 .00000069 00000-0 55566-4 0 9994
2 11378 82.9437 253.1280 0033681 45.9182 16.2957 13.75834616192349
| Epoch (UTC): | 02 February 2023 13:30:24 |
| Eccentricity: | 0.0033681 |
| inclination: | 82.9437° |
| perigee height: | 954 km |
| apogee height: | 1003 km |
| right ascension of ascending node: | 253.1280° |
| argument of perigee: | 45.9182° |
| revolutions per day: | 13.75834616 |
| mean anomaly at epoch: | 16.2957° |
| orbit number at epoch: | 19234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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