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 19120U 88039B 23150.14148981 .00000023 00000-0 33803-4 0 9994
2 19120 71.0160 53.2960 0019718 96.9378 263.3991 14.19316079814684
| Epoch (UTC): | 30 May 2023 03:23:44 |
| Eccentricity: | 0.0019718 |
| inclination: | 71.0160° |
| perigee height: | 813 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 53.2960° |
| argument of perigee: | 96.9378° |
| revolutions per day: | 14.19316079 |
| mean anomaly at epoch: | 263.3991° |
| orbit number at epoch: | 81468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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