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 48786U 21045V 24358.10558477 .00000175 00000-0 43178-3 0 9993
2 48786 87.9066 6.8997 0001624 85.0527 275.0789 13.15550124174254
| Epoch (UTC): | 23 December 2024 02:32:02 |
| Eccentricity: | 0.0001624 |
| inclination: | 87.9066° |
| perigee height: | 1200 km |
| apogee height: | 1203 km |
| right ascension of ascending node: | 6.8997° |
| argument of perigee: | 85.0527° |
| revolutions per day: | 13.15550124 |
| mean anomaly at epoch: | 275.0789° |
| orbit number at epoch: | 17425 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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