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 is defined by the following mean orbital elements,
1 27387U 26073.61688803 +.00000000 +00000-0 +55570-4 0 00004
2 27387 98.8154 89.5443 0032861 46.6827 313.7090 14.36772853 09
| Epoch (UTC): | 14 March 2026 14:48:19 |
| Eccentricity: | 0.0032861 |
| inclination: | 98.8154° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 89.5443° |
| argument of perigee: | 46.6827° |
| revolutions per day: | 14.36772853 |
| mean anomaly at epoch: | 313.7090° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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