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 66916U 26145.53859157 +.00000000 +00000-0 +33958-4 0 00004
2 66916 50.0057 227.3906 0001131 211.8330 148.2474 13.29322789 06
| Epoch (UTC): | 25 May 2026 12:55:34 |
| Eccentricity: | 0.0001131 |
| inclination: | 50.0057° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.3906° |
| argument of perigee: | 211.8330° |
| revolutions per day: | 13.29322789 |
| mean anomaly at epoch: | 148.2474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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