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 65418U 26145.62833853 +.00000000 +00000-0 +41468-3 0 00009
2 65418 53.1580 234.9956 0001189 98.7215 261.3921 15.30209638 08
| Epoch (UTC): | 25 May 2026 15:04:48 |
| Eccentricity: | 0.0001189 |
| inclination: | 53.1580° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.9956° |
| argument of perigee: | 98.7215° |
| revolutions per day: | 15.30209638 |
| mean anomaly at epoch: | 261.3921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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