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 28352U 26021.48567431 +.00000000 +00000-0 -86515-4 0 00002
2 28352 71.0051 46.1182 0011513 343.2513 16.8226 14.12162234 01
| Epoch (UTC): | 21 January 2026 11:39:22 |
| Eccentricity: | 0.0011513 |
| inclination: | 71.0051° |
| perigee height: | 844 km |
| apogee height: | 860 km |
| right ascension of ascending node: | 46.1182° |
| argument of perigee: | 343.2513° |
| revolutions per day: | 14.12162234 |
| mean anomaly at epoch: | 16.8226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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