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 24262.47237975 .00000345 00000-0 17002-3 0 9995
2 25397 98.9334 230.6375 0000408 192.1661 167.9507 14.24125727360692
| Epoch (UTC): | 18 September 2024 11:20:13 |
| Eccentricity: | 0.0000408 |
| inclination: | 98.9334° |
| perigee height: | 811 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 230.6375° |
| argument of perigee: | 192.1661° |
| revolutions per day: | 14.24125727 |
| mean anomaly at epoch: | 167.9507° |
| orbit number at epoch: | 36069 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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