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 26076.33284618 +.00000000 +00000-0 +44390-4 0 00000
2 27387 98.8153 92.3250 0032745 38.8735 321.4797 14.36773487 02
| Epoch (UTC): | 17 March 2026 07:59:17 |
| Eccentricity: | 0.0032745 |
| inclination: | 98.8153° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 92.3250° |
| argument of perigee: | 38.8735° |
| revolutions per day: | 14.36773487 |
| mean anomaly at epoch: | 321.4797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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