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 49141U 26145.61727480 +.00000000 +00000-0 -33126-4 0 00005
2 49141 69.9994 100.5047 0003394 266.0119 94.0652 14.98325715 09
| Epoch (UTC): | 25 May 2026 14:48:52 |
| Eccentricity: | 0.0003394 |
| inclination: | 69.9994° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 100.5047° |
| argument of perigee: | 266.0119° |
| revolutions per day: | 14.98325715 |
| mean anomaly at epoch: | 94.0652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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