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 13148U 82037A 24357.51597591 .00000304 00000-0 12154-3 0 9993
2 13148 74.0383 14.6114 0010356 310.3615 49.6631 14.32546803227483
| Epoch (UTC): | 22 December 2024 12:23:00 |
| Eccentricity: | 0.0010356 |
| inclination: | 74.0383° |
| perigee height: | 776 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 14.6114° |
| argument of perigee: | 310.3615° |
| revolutions per day: | 14.32546803 |
| mean anomaly at epoch: | 49.6631° |
| orbit number at epoch: | 22748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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