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 66895U 26145.41016403 +.00000000 +00000-0 +84771-3 0 00004
2 66895 53.1593 27.5782 0001040 87.3888 272.7233 15.34403569 06
| Epoch (UTC): | 25 May 2026 09:50:38 |
| Eccentricity: | 0.0001040 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 27.5782° |
| argument of perigee: | 87.3888° |
| revolutions per day: | 15.34403569 |
| mean anomaly at epoch: | 272.7233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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