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 66121U 26145.40817237 +.00000000 +00000-0 +50524-3 0 00008
2 66121 53.1570 43.4737 0001023 82.9060 277.2057 15.30211422 09
| Epoch (UTC): | 25 May 2026 09:47:46 |
| Eccentricity: | 0.0001023 |
| inclination: | 53.1570° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 43.4737° |
| argument of perigee: | 82.9060° |
| revolutions per day: | 15.30211422 |
| mean anomaly at epoch: | 277.2057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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