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 26072.38743263 +.00000000 +00000-0 +62281-4 0 00005
2 27386 98.3733 25.8968 0001324 83.1865 85.2937 14.39038451 02
| Epoch (UTC): | 13 March 2026 09:17:54 |
| Eccentricity: | 0.0001324 |
| inclination: | 98.3733° |
| perigee height: | 761 km |
| apogee height: | 763 km |
| right ascension of ascending node: | 25.8968° |
| argument of perigee: | 83.1865° |
| revolutions per day: | 14.39038451 |
| mean anomaly at epoch: | 85.2937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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