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 65047U 26145.57841360 +.00000000 +00000-0 +76326-4 0 00005
2 65047 50.0031 346.7841 0000861 161.8756 198.2147 13.29315293 05
| Epoch (UTC): | 25 May 2026 13:52:54 |
| Eccentricity: | 0.0000861 |
| inclination: | 50.0031° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 346.7841° |
| argument of perigee: | 161.8756° |
| revolutions per day: | 13.29315293 |
| mean anomaly at epoch: | 198.2147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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