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 21875U 92008A 23334.13959265 .00000097 00000-0 86583-4 0 9997
2 21875 82.9278 190.7296 0038478 41.4720 72.6022 13.73832496593353
| Epoch (UTC): | 30 November 2023 03:21:00 |
| Eccentricity: | 0.0038478 |
| inclination: | 82.9278° |
| perigee height: | 957 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 190.7296° |
| argument of perigee: | 41.4720° |
| revolutions per day: | 13.73832496 |
| mean anomaly at epoch: | 72.6022° |
| orbit number at epoch: | 59335 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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