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 26133.42467314 +.00000000 +00000-0 +27026-4 0 00006
2 27386 98.3817 85.5230 0001193 91.4361 21.8484 14.39056310 04
| Epoch (UTC): | 13 May 2026 10:11:31 |
| Eccentricity: | 0.0001193 |
| inclination: | 98.3817° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 85.5230° |
| argument of perigee: | 91.4361° |
| revolutions per day: | 14.39056310 |
| mean anomaly at epoch: | 21.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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