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 25400U 98043G 22228.43873322 .00000021 00000-0 27285-4 0 9994
2 25400 98.6731 163.9097 0009627 188.2688 171.8335 14.25523549253566
| Epoch (UTC): | 16 August 2022 10:31:46 |
| Eccentricity: | 0.0009627 |
| inclination: | 98.6731° |
| perigee height: | 800 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 163.9097° |
| argument of perigee: | 188.2688° |
| revolutions per day: | 14.25523549 |
| mean anomaly at epoch: | 171.8335° |
| orbit number at epoch: | 25356 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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