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 26930U 26053.58086338 +.00000000 +00000-0 +60641-4 0 00001
2 26930 67.0006 121.7486 0009084 299.0449 60.9742 14.31554714 01
| Epoch (UTC): | 22 February 2026 13:56:26 |
| Eccentricity: | 0.0009084 |
| inclination: | 67.0006° |
| perigee height: | 780 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 121.7486° |
| argument of perigee: | 299.0449° |
| revolutions per day: | 14.31554714 |
| mean anomaly at epoch: | 60.9742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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