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 65619U 26145.49847700 +.00000000 +00000-0 +15333-3 0 00005
2 65619 49.9996 81.7302 0002313 39.6902 320.4145 13.41459446 04
| Epoch (UTC): | 25 May 2026 11:57:48 |
| Eccentricity: | 0.0002313 |
| inclination: | 49.9996° |
| perigee height: | 1102 km |
| apogee height: | 1106 km |
| right ascension of ascending node: | 81.7302° |
| argument of perigee: | 39.6902° |
| revolutions per day: | 13.41459446 |
| mean anomaly at epoch: | 320.4145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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