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 13992U 26070.83321639 +.00000000 +00000-0 +71854-4 0 00006
2 13992 74.0504 273.1438 0005226 192.5149 167.5876 14.37553787 00
| Epoch (UTC): | 11 March 2026 19:59:49 |
| Eccentricity: | 0.0005226 |
| inclination: | 74.0504° |
| perigee height: | 763 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 273.1438° |
| argument of perigee: | 192.5149° |
| revolutions per day: | 14.37553787 |
| mean anomaly at epoch: | 167.5876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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