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 25397U 98043D 22175.80774700 .00000020 00000-0 28494-4 0 9993
2 25397 98.8183 126.2954 0002409 86.9190 273.2264 14.23758663244474
| Epoch (UTC): | 24 June 2022 19:23:09 |
| Eccentricity: | 0.0002409 |
| inclination: | 98.8183° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 126.2954° |
| argument of perigee: | 86.9190° |
| revolutions per day: | 14.23758663 |
| mean anomaly at epoch: | 273.2264° |
| orbit number at epoch: | 24447 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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