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 22177.89134893 .00000158 00000-0 84273-4 0 9997
2 25338 98.6430 207.3033 0009148 269.9664 90.0468 14.26143168254368
| Epoch (UTC): | 26 June 2022 21:23:32 |
| Eccentricity: | 0.0009148 |
| inclination: | 98.6430° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 207.3033° |
| argument of perigee: | 269.9664° |
| revolutions per day: | 14.26143168 |
| mean anomaly at epoch: | 90.0468° |
| orbit number at epoch: | 25436 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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