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 66535U 26145.47843594 +.00000000 +00000-0 +48429-3 0 00000
2 66535 43.0038 204.5859 0001313 282.7099 77.3606 15.27575848 04
| Epoch (UTC): | 25 May 2026 11:28:56 |
| Eccentricity: | 0.0001313 |
| inclination: | 43.0038° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.5859° |
| argument of perigee: | 282.7099° |
| revolutions per day: | 15.27575848 |
| mean anomaly at epoch: | 77.3606° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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