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 27431U 26053.70520969 +.00000000 +00000-0 +85479-4 0 00001
2 27431 98.9694 104.4761 0015076 201.4523 158.6017 14.10206715 08
| Epoch (UTC): | 22 February 2026 16:55:30 |
| Eccentricity: | 0.0015076 |
| inclination: | 98.9694° |
| perigee height: | 848 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 104.4761° |
| argument of perigee: | 201.4523° |
| revolutions per day: | 14.10206715 |
| mean anomaly at epoch: | 158.6017° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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