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 66021U 26145.61850008 +.00000000 +00000-0 +15498-3 0 00004
2 66021 53.1575 106.5815 0001853 102.9245 257.1962 15.30208581 04
| Epoch (UTC): | 25 May 2026 14:50:38 |
| Eccentricity: | 0.0001853 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.5815° |
| argument of perigee: | 102.9245° |
| revolutions per day: | 15.30208581 |
| mean anomaly at epoch: | 257.1962° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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