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 26067.97604366 +.00000000 +00000-0 +57216-4 0 00007
2 27387 98.8158 83.7689 0033029 62.8835 297.5712 14.36771047 01
| Epoch (UTC): | 08 March 2026 23:25:30 |
| Eccentricity: | 0.0033029 |
| inclination: | 98.8158° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 83.7689° |
| argument of perigee: | 62.8835° |
| revolutions per day: | 14.36771047 |
| mean anomaly at epoch: | 297.5712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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