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 26133.45347609 +.00000000 +00000-0 +52195-4 0 00004
2 05485 32.0544 253.4229 0639380 169.4443 192.0295 12.74249793 05
| Epoch (UTC): | 13 May 2026 10:53:00 |
| Eccentricity: | 0.0639380 |
| inclination: | 32.0544° |
| perigee height: | 870 km |
| apogee height: | 1860 km |
| right ascension of ascending node: | 253.4229° |
| argument of perigee: | 169.4443° |
| revolutions per day: | 12.74249793 |
| mean anomaly at epoch: | 192.0295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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