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 66093U 26145.61742683 +.00000000 +00000-0 +15131-3 0 00006
2 66093 53.1576 106.4703 0001416 101.8430 258.2730 15.30209162 09
| Epoch (UTC): | 25 May 2026 14:49:05 |
| Eccentricity: | 0.0001416 |
| inclination: | 53.1576° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 106.4703° |
| argument of perigee: | 101.8430° |
| revolutions per day: | 15.30209162 |
| mean anomaly at epoch: | 258.2730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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