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 22177.54055380 .00000164 00000-0 86753-4 0 9994
2 25338 98.6430 206.9571 0009143 271.1449 88.8684 14.26143054254315
| Epoch (UTC): | 26 June 2022 12:58:23 |
| Eccentricity: | 0.0009143 |
| inclination: | 98.6430° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 206.9571° |
| argument of perigee: | 271.1449° |
| revolutions per day: | 14.26143054 |
| mean anomaly at epoch: | 88.8684° |
| orbit number at epoch: | 25431 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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