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 26032.12662955 +.00000000 +00000-0 -91117-5 0 00009
2 05485 32.0590 331.8634 0640171 219.4593 135.7652 12.74248690 05
| Epoch (UTC): | 01 February 2026 03:02:20 |
| Eccentricity: | 0.0640171 |
| inclination: | 32.0590° |
| perigee height: | 869 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 331.8634° |
| argument of perigee: | 219.4593° |
| revolutions per day: | 12.74248690 |
| mean anomaly at epoch: | 135.7652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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