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 23079.11673532 .00000198 00000-0 10632-3 0 9992
2 25397 98.8585 35.8567 0002149 58.2736 301.8651 14.23841723282878
| Epoch (UTC): | 20 March 2023 02:48:05 |
| Eccentricity: | 0.0002149 |
| inclination: | 98.8585° |
| perigee height: | 811 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 35.8567° |
| argument of perigee: | 58.2736° |
| revolutions per day: | 14.23841723 |
| mean anomaly at epoch: | 301.8651° |
| orbit number at epoch: | 28287 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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