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 01293U 26068.59315093 +.00000000 +00000-0 +18182-3 0 00008
2 01293 70.0713 255.8316 0019742 278.9493 80.9385 14.08393500 06
| Epoch (UTC): | 09 March 2026 14:14:08 |
| Eccentricity: | 0.0019742 |
| inclination: | 70.0713° |
| perigee height: | 851 km |
| apogee height: | 879 km |
| right ascension of ascending node: | 255.8316° |
| argument of perigee: | 278.9493° |
| revolutions per day: | 14.08393500 |
| mean anomaly at epoch: | 80.9385° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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