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 00107U 61013A 22027.30592648 .00000606 00000-0 63419-4 0 9998
2 00107 28.7869 94.6328 0544664 87.2147 279.0607 14.09528547 49368
| Epoch (UTC): | 27 January 2022 07:20:32 |
| Eccentricity: | 0.0544664 |
| inclination: | 28.7869° |
| perigee height: | 467 km |
| apogee height: | 1255 km |
| right ascension of ascending node: | 94.6328° |
| argument of perigee: | 87.2147° |
| revolutions per day: | 14.09528547 |
| mean anomaly at epoch: | 279.0607° |
| orbit number at epoch: | 4936 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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