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 26072.01625762 +.00000000 +00000-0 +90272-4 0 00007
2 13992 74.0503 270.9682 0005183 189.8547 170.2506 14.37554740 09
| Epoch (UTC): | 13 March 2026 00:23:24 |
| Eccentricity: | 0.0005183 |
| inclination: | 74.0503° |
| perigee height: | 763 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 270.9682° |
| argument of perigee: | 189.8547° |
| revolutions per day: | 14.37554740 |
| mean anomaly at epoch: | 170.2506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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