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 66896U 26145.40693377 +.00000000 +00000-0 +86091-3 0 00002
2 66896 53.1605 27.5556 0001358 82.9017 277.2139 15.30209743 06
| Epoch (UTC): | 25 May 2026 09:45:59 |
| Eccentricity: | 0.0001358 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 27.5556° |
| argument of perigee: | 82.9017° |
| revolutions per day: | 15.30209743 |
| mean anomaly at epoch: | 277.2139° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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