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 05104U 26053.73187823 +.00000000 +00000-0 +84520-4 0 00001
2 05104 88.1752 334.6201 0044893 39.6298 16.7304 12.67883852 08
| Epoch (UTC): | 22 February 2026 17:33:54 |
| Eccentricity: | 0.0044893 |
| inclination: | 88.1752° |
| perigee height: | 1356 km |
| apogee height: | 1425 km |
| right ascension of ascending node: | 334.6201° |
| argument of perigee: | 39.6298° |
| revolutions per day: | 12.67883852 |
| mean anomaly at epoch: | 16.7304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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