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 66028U 26145.30564257 +.00000000 +00000-0 +67623-3 0 00002
2 66028 53.1581 108.1791 0001266 81.1696 278.9448 15.30208424 01
| Epoch (UTC): | 25 May 2026 07:20:07 |
| Eccentricity: | 0.0001266 |
| inclination: | 53.1581° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.1791° |
| argument of perigee: | 81.1696° |
| revolutions per day: | 15.30208424 |
| mean anomaly at epoch: | 278.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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