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 27940U 26038.05020763 +.00000000 +00000-0 +18686-3 0 00009
2 27940 98.3769 212.6050 0013912 50.4593 309.7838 14.69316292 05
| Epoch (UTC): | 07 February 2026 01:12:17 |
| Eccentricity: | 0.0013912 |
| inclination: | 98.3769° |
| perigee height: | 653 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 212.6050° |
| argument of perigee: | 50.4593° |
| revolutions per day: | 14.69316292 |
| mean anomaly at epoch: | 309.7838° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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