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 27859U 03036B 24357.82628425 .00003505 00000-0 41136-3 0 9992
2 27859 73.9270 99.5615 0008010 324.5834 35.4812 14.85348990153333
| Epoch (UTC): | 22 December 2024 19:49:50 |
| Eccentricity: | 0.0008010 |
| inclination: | 73.9270° |
| perigee height: | 607 km |
| apogee height: | 618 km |
| right ascension of ascending node: | 99.5615° |
| argument of perigee: | 324.5834° |
| revolutions per day: | 14.85348990 |
| mean anomaly at epoch: | 35.4812° |
| orbit number at epoch: | 15333 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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