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 05485U 26053.83476743 +.00000000 +00000-0 +21554-5 0 00005
2 05485 32.0526 237.9368 0639900 2.9325 357.4779 12.74248471 00
| Epoch (UTC): | 22 February 2026 20:02:03 |
| Eccentricity: | 0.0639900 |
| inclination: | 32.0526° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 237.9368° |
| argument of perigee: | 2.9325° |
| revolutions per day: | 12.74248471 |
| mean anomaly at epoch: | 357.4779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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