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 22094.50210998 .00000364 00000-0 91231-4 0 9992
2 44874 98.2389 282.3781 0010476 197.7420 162.3414 14.56937393122025
| Epoch (UTC): | 04 April 2022 12:03:02 |
| Eccentricity: | 0.0010476 |
| inclination: | 98.2389° |
| perigee height: | 695 km |
| apogee height: | 710 km |
| right ascension of ascending node: | 282.3781° |
| argument of perigee: | 197.7420° |
| revolutions per day: | 14.56937393 |
| mean anomaly at epoch: | 162.3414° |
| orbit number at epoch: | 12202 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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