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 22179.15421128 .00000121 00000-0 68830-4 0 9999
2 25338 98.6429 208.5496 0009152 265.7767 94.2367 14.26143508254794
| Epoch (UTC): | 28 June 2022 03:42:03 |
| Eccentricity: | 0.0009152 |
| inclination: | 98.6429° |
| perigee height: | 798 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 208.5496° |
| argument of perigee: | 265.7767° |
| revolutions per day: | 14.26143508 |
| mean anomaly at epoch: | 94.2367° |
| orbit number at epoch: | 25479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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