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 63665U 26145.41560166 +.00000000 +00000-0 +14493-2 0 00009
2 63665 42.9982 175.5062 0000870 124.4692 235.6258 15.71000502 03
| Epoch (UTC): | 25 May 2026 09:58:27 |
| Eccentricity: | 0.0000870 |
| inclination: | 42.9982° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 175.5062° |
| argument of perigee: | 124.4692° |
| revolutions per day: | 15.71000502 |
| mean anomaly at epoch: | 235.6258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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