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 26045.86631954 +.00000000 +00000-0 +55207-4 0 00001
2 27386 98.3689 0.0128 0001353 87.4996 287.4248 14.39028210 02
| Epoch (UTC): | 14 February 2026 20:47:30 |
| Eccentricity: | 0.0001353 |
| inclination: | 98.3689° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 0.0128° |
| argument of perigee: | 87.4996° |
| revolutions per day: | 14.39028210 |
| mean anomaly at epoch: | 287.4248° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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