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 27386U 26135.84042816 +.00000000 +00000-0 +20841-4 0 00008
2 27386 98.3819 87.8841 0001204 91.7401 289.3659 14.39056569 01
| Epoch (UTC): | 15 May 2026 20:10:12 |
| Eccentricity: | 0.0001204 |
| inclination: | 98.3819° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 87.8841° |
| argument of perigee: | 91.7401° |
| revolutions per day: | 14.39056569 |
| mean anomaly at epoch: | 289.3659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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