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 65618U 26145.50120934 +.00000000 +00000-0 +93645-4 0 00002
2 65618 49.9994 82.3886 0001866 28.6503 331.4477 13.41461715 04
| Epoch (UTC): | 25 May 2026 12:01:44 |
| Eccentricity: | 0.0001866 |
| inclination: | 49.9994° |
| perigee height: | 1102 km |
| apogee height: | 1105 km |
| right ascension of ascending node: | 82.3886° |
| argument of perigee: | 28.6503° |
| revolutions per day: | 13.41461715 |
| mean anomaly at epoch: | 331.4477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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