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 26064.98151647 +.00000000 +00000-0 +53504-4 0 00000
2 27387 98.8158 80.7029 0033088 71.4753 289.0023 14.36769909 01
| Epoch (UTC): | 05 March 2026 23:33:23 |
| Eccentricity: | 0.0033088 |
| inclination: | 98.8158° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 80.7029° |
| argument of perigee: | 71.4753° |
| revolutions per day: | 14.36769909 |
| mean anomaly at epoch: | 289.0023° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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