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 13649U 26020.33956036 +.00000000 +00000-0 +11476-3 0 00003
2 13649 74.0016 342.8678 0017029 125.5871 343.3366 14.38582249 03
| Epoch (UTC): | 20 January 2026 08:08:58 |
| Eccentricity: | 0.0017029 |
| inclination: | 74.0016° |
| perigee height: | 751 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 342.8678° |
| argument of perigee: | 125.5871° |
| revolutions per day: | 14.38582249 |
| mean anomaly at epoch: | 343.3366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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