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 10954U 78062B 21022.97867351 .00000097 00000-0 24594-8 0 9993
2 10954 28.4267 118.7800 0698350 63.9532 303.1219 13.50990169 94728
| Epoch (UTC): | 22 January 2021 23:29:17 |
| Eccentricity: | 0.0698350 |
| inclination: | 28.4267° |
| perigee height: | 548 km |
| apogee height: | 1588 km |
| right ascension of ascending node: | 118.7800° |
| argument of perigee: | 63.9532° |
| revolutions per day: | 13.50990169 |
| mean anomaly at epoch: | 303.1219° |
| orbit number at epoch: | 9472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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