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 25397U 98043D 23158.73389885 .00000112 00000-0 68602-4 0 9990
2 25397 98.8682 116.1086 0001932 128.0844 232.0508 14.23876285294207
| Epoch (UTC): | 07 June 2023 17:36:48 |
| Eccentricity: | 0.0001932 |
| inclination: | 98.8682° |
| perigee height: | 811 km |
| apogee height: | 813 km |
| right ascension of ascending node: | 116.1086° |
| argument of perigee: | 128.0844° |
| revolutions per day: | 14.23876285 |
| mean anomaly at epoch: | 232.0508° |
| orbit number at epoch: | 29420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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