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 26109.30907535 +.00000000 +00000-0 +31401-4 0 00002
2 27386 98.3791 61.9565 0001151 85.4373 87.1097 14.39050190 09
| Epoch (UTC): | 19 April 2026 07:25:04 |
| Eccentricity: | 0.0001151 |
| inclination: | 98.3791° |
| perigee height: | 761 km |
| apogee height: | 762 km |
| right ascension of ascending node: | 61.9565° |
| argument of perigee: | 85.4373° |
| revolutions per day: | 14.39050190 |
| mean anomaly at epoch: | 87.1097° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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