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 28420U 26145.63422159 +.00000000 +00000-0 +47535-3 0 00006
2 28420 82.4860 343.2141 0013264 333.1611 26.8782 12.45323387 09
| Epoch (UTC): | 25 May 2026 15:13:16 |
| Eccentricity: | 0.0013264 |
| inclination: | 82.4860° |
| perigee height: | 1474 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 343.2141° |
| argument of perigee: | 333.1611° |
| revolutions per day: | 12.45323387 |
| mean anomaly at epoch: | 26.8782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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