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 06153U 26053.64430663 +.00000000 +00000-0 +86875-4 0 00004
2 06153 35.0067 23.0323 0006186 33.1256 142.7810 14.59983807 09
| Epoch (UTC): | 22 February 2026 15:27:48 |
| Eccentricity: | 0.0006186 |
| inclination: | 35.0067° |
| perigee height: | 689 km |
| apogee height: | 698 km |
| right ascension of ascending node: | 23.0323° |
| argument of perigee: | 33.1256° |
| revolutions per day: | 14.59983807 |
| mean anomaly at epoch: | 142.7810° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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