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 25544U 98067A 22092.17989097 .00019620 00000-0 35347-3 0 9998
2 25544 51.6448 353.0512 0004600 338.3217 118.2786 15.49785171333398
| Epoch (UTC): | 02 April 2022 04:19:02 |
| Eccentricity: | 0.0004600 |
| inclination: | 51.6448° |
| perigee height: | 414 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 353.0512° |
| argument of perigee: | 338.3217° |
| revolutions per day: | 15.49785171 |
| mean anomaly at epoch: | 118.2786° |
| orbit number at epoch: | 33339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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