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 26065.05718365 +.00000000 +00000-0 +10031-3 0 00009
2 13992 74.0508 283.7645 0005467 203.7847 156.3055 14.37551061 06
| Epoch (UTC): | 06 March 2026 01:22:20 |
| Eccentricity: | 0.0005467 |
| inclination: | 74.0508° |
| perigee height: | 763 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 283.7645° |
| argument of perigee: | 203.7847° |
| revolutions per day: | 14.37551061 |
| mean anomaly at epoch: | 156.3055° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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