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 26074.52220772 +.00000000 +00000-0 +45918-4 0 00007
2 27387 98.8154 90.4712 0032824 44.0841 316.2953 14.36772982 05
| Epoch (UTC): | 15 March 2026 12:31:58 |
| Eccentricity: | 0.0032824 |
| inclination: | 98.8154° |
| perigee height: | 746 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 90.4712° |
| argument of perigee: | 44.0841° |
| revolutions per day: | 14.36772982 |
| mean anomaly at epoch: | 316.2953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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