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 24259.87283226 .00000550 00000-0 25889-3 0 9995
2 25397 98.9327 227.9956 0000279 211.1889 148.9273 14.24124046360320
| Epoch (UTC): | 15 September 2024 20:56:52 |
| Eccentricity: | 0.0000279 |
| inclination: | 98.9327° |
| perigee height: | 811 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 227.9956° |
| argument of perigee: | 211.1889° |
| revolutions per day: | 14.24124046 |
| mean anomaly at epoch: | 148.9273° |
| orbit number at epoch: | 36032 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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