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 25338U 98030A 22176.55832742 .00000137 00000-0 75651-4 0 9994
2 25338 98.6431 205.9878 0009139 274.4055 85.6080 14.26142502254175
| Epoch (UTC): | 25 June 2022 13:23:59 |
| Eccentricity: | 0.0009139 |
| inclination: | 98.6431° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 205.9878° |
| argument of perigee: | 274.4055° |
| revolutions per day: | 14.26142502 |
| mean anomaly at epoch: | 85.6080° |
| orbit number at epoch: | 25417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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