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 27561U 26041.60722189 +.00000000 +00000-0 +11205-3 0 00004
2 27561 98.4747 259.9076 0044579 159.3468 200.9545 14.58459156 08
| Epoch (UTC): | 10 February 2026 14:34:23 |
| Eccentricity: | 0.0044579 |
| inclination: | 98.4747° |
| perigee height: | 667 km |
| apogee height: | 730 km |
| right ascension of ascending node: | 259.9076° |
| argument of perigee: | 159.3468° |
| revolutions per day: | 14.58459156 |
| mean anomaly at epoch: | 200.9545° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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