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 25261U 98017B 24357.99061664 .00001001 00000-0 36320-3 0 9992
2 25261 98.8502 4.3074 0002473 286.6375 73.4538 14.35643041398563
| Epoch (UTC): | 22 December 2024 23:46:29 |
| Eccentricity: | 0.0002473 |
| inclination: | 98.8502° |
| perigee height: | 771 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 4.3074° |
| argument of perigee: | 286.6375° |
| revolutions per day: | 14.35643041 |
| mean anomaly at epoch: | 73.4538° |
| orbit number at epoch: | 39856 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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