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 26133.42652411 +.00000000 +00000-0 +13460-3 0 00000
2 05104 88.1637 321.9059 0043262 198.1506 177.2671 12.67885313 06
| Epoch (UTC): | 13 May 2026 10:14:11 |
| Eccentricity: | 0.0043262 |
| inclination: | 88.1637° |
| perigee height: | 1357 km |
| apogee height: | 1424 km |
| right ascension of ascending node: | 321.9059° |
| argument of perigee: | 198.1506° |
| revolutions per day: | 12.67885313 |
| mean anomaly at epoch: | 177.2671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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