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 26162.55225253 +.00000000 +00000-0 +59206-4 0 00009
2 13992 74.0521 104.5056 0005229 337.0196 23.0723 14.37597508 09
| Epoch (UTC): | 11 June 2026 13:15:14 |
| Eccentricity: | 0.0005229 |
| inclination: | 74.0521° |
| perigee height: | 763 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 104.5056° |
| argument of perigee: | 337.0196° |
| revolutions per day: | 14.37597508 |
| mean anomaly at epoch: | 23.0723° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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