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 25634U 99008A 22181.59458108 .00000000 00000-0 19341-4 0 9992
2 25634 98.3929 195.1216 0008982 283.5228 76.4949 14.19438769208904
| Epoch (UTC): | 30 June 2022 14:16:11 |
| Eccentricity: | 0.0008982 |
| inclination: | 98.3929° |
| perigee height: | 821 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 195.1216° |
| argument of perigee: | 283.5228° |
| revolutions per day: | 14.19438769 |
| mean anomaly at epoch: | 76.4949° |
| orbit number at epoch: | 20890 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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