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 24251.93364214 .00000641 00000-0 29872-3 0 9998
2 25397 98.9309 219.9280 0000340 329.2073 30.9085 14.24114699359193
| Epoch (UTC): | 07 September 2024 22:24:26 |
| Eccentricity: | 0.0000340 |
| inclination: | 98.9309° |
| perigee height: | 811 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 219.9280° |
| argument of perigee: | 329.2073° |
| revolutions per day: | 14.24114699 |
| mean anomaly at epoch: | 30.9085° |
| orbit number at epoch: | 35919 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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