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 44874U 19092B 22014.56019136 .00000093 00000-0 30848-4 0 9997
2 44874 98.2344 203.3398 0012126 91.7387 268.5200 14.56901901110386
| Epoch (UTC): | 14 January 2022 13:26:40 |
| Eccentricity: | 0.0012126 |
| inclination: | 98.2344° |
| perigee height: | 694 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 203.3398° |
| argument of perigee: | 91.7387° |
| revolutions per day: | 14.56901901 |
| mean anomaly at epoch: | 268.5200° |
| orbit number at epoch: | 11038 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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