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 25756U 26053.63477999 +.00000000 +00000-0 +67461-4 0 00006
2 25756 98.6324 85.4422 0012150 251.5299 108.4578 14.55734472 01
| Epoch (UTC): | 22 February 2026 15:14:04 |
| Eccentricity: | 0.0012150 |
| inclination: | 98.6324° |
| perigee height: | 698 km |
| apogee height: | 716 km |
| right ascension of ascending node: | 85.4422° |
| argument of perigee: | 251.5299° |
| revolutions per day: | 14.55734472 |
| mean anomaly at epoch: | 108.4578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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