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 26064.70922947 +.00000000 +00000-0 +11486-3 0 00008
2 13992 74.0508 284.4043 0005471 204.2976 155.7921 14.37551106 05
| Epoch (UTC): | 05 March 2026 17:01:17 |
| Eccentricity: | 0.0005471 |
| inclination: | 74.0508° |
| perigee height: | 763 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 284.4043° |
| argument of perigee: | 204.2976° |
| revolutions per day: | 14.37551106 |
| mean anomaly at epoch: | 155.7921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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