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 26127.84627743 +.00000000 +00000-0 +42121-4 0 00002
2 27386 98.3810 80.0708 0001159 90.5096 300.0651 14.39055208 07
| Epoch (UTC): | 07 May 2026 20:18:38 |
| Eccentricity: | 0.0001159 |
| inclination: | 98.3810° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 80.0708° |
| argument of perigee: | 90.5096° |
| revolutions per day: | 14.39055208 |
| mean anomaly at epoch: | 300.0651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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