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 66891U 26144.96978104 +.00000000 +00000-0 +34502-3 0 00001
2 66891 53.1581 29.8036 0000897 79.9731 280.1371 15.30204844 06
| Epoch (UTC): | 24 May 2026 23:16:29 |
| Eccentricity: | 0.0000897 |
| inclination: | 53.1581° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 29.8036° |
| argument of perigee: | 79.9731° |
| revolutions per day: | 15.30204844 |
| mean anomaly at epoch: | 280.1371° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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