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 22069.77798350 .00000179 00000-0 50017-4 0 9997
2 44874 98.2380 257.9297 0009699 282.0736 77.9375 14.56922988118429
| Epoch (UTC): | 10 March 2022 18:40:17 |
| Eccentricity: | 0.0009699 |
| inclination: | 98.2380° |
| perigee height: | 696 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 257.9297° |
| argument of perigee: | 282.0736° |
| revolutions per day: | 14.56922988 |
| mean anomaly at epoch: | 77.9375° |
| orbit number at epoch: | 11842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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