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 22018.54359334 .00000122 00000-0 37355-4 0 9999
2 44874 98.2345 207.2772 0012110 80.6726 279.5841 14.56903388110961
| Epoch (UTC): | 18 January 2022 13:02:46 |
| Eccentricity: | 0.0012110 |
| inclination: | 98.2345° |
| perigee height: | 694 km |
| apogee height: | 712 km |
| right ascension of ascending node: | 207.2772° |
| argument of perigee: | 80.6726° |
| revolutions per day: | 14.56903388 |
| mean anomaly at epoch: | 279.5841° |
| orbit number at epoch: | 11096 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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