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 26074.52151873 +.00000000 +00000-0 +96934-4 0 00003
2 13992 74.0502 266.3613 0005105 184.7685 175.3421 14.37556547 01
| Epoch (UTC): | 15 March 2026 12:30:59 |
| Eccentricity: | 0.0005105 |
| inclination: | 74.0502° |
| perigee height: | 763 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 266.3613° |
| argument of perigee: | 184.7685° |
| revolutions per day: | 14.37556547 |
| mean anomaly at epoch: | 175.3421° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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