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 26141.26657956 +.00000000 +00000-0 +28953-4 0 00007
2 13649 73.9980 119.4352 0019206 233.1454 231.0785 14.38651233 08
| Epoch (UTC): | 21 May 2026 06:23:52 |
| Eccentricity: | 0.0019206 |
| inclination: | 73.9980° |
| perigee height: | 749 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 119.4352° |
| argument of perigee: | 233.1454° |
| revolutions per day: | 14.38651233 |
| mean anomaly at epoch: | 231.0785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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