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 65416U 26145.53252937 +.00000000 +00000-0 +11538-3 0 00000
2 65416 53.1567 235.8147 0001094 86.5999 273.5127 15.30197423 03
| Epoch (UTC): | 25 May 2026 12:46:50 |
| Eccentricity: | 0.0001094 |
| inclination: | 53.1567° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.8147° |
| argument of perigee: | 86.5999° |
| revolutions per day: | 15.30197423 |
| mean anomaly at epoch: | 273.5127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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