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 66893U 26145.40071183 +.00000000 +00000-0 +16926-3 0 00004
2 66893 53.1616 28.2274 0002302 80.8138 279.3123 15.30211787 08
| Epoch (UTC): | 25 May 2026 09:37:01 |
| Eccentricity: | 0.0002302 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 28.2274° |
| argument of perigee: | 80.8138° |
| revolutions per day: | 15.30211787 |
| mean anomaly at epoch: | 279.3123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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