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 25860U 99039A 23332.69914040 .00001654 00000-0 23700-3 0 9998
2 25860 98.0674 20.1523 0001671 107.2263 252.9131 14.77915857311390
| Epoch (UTC): | 28 November 2023 16:46:45 |
| Eccentricity: | 0.0001671 |
| inclination: | 98.0674° |
| perigee height: | 635 km |
| apogee height: | 637 km |
| right ascension of ascending node: | 20.1523° |
| argument of perigee: | 107.2263° |
| revolutions per day: | 14.77915857 |
| mean anomaly at epoch: | 252.9131° |
| orbit number at epoch: | 31139 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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