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 63468U 26145.57038566 +.00000000 +00000-0 +56240-3 0 00008
2 63468 43.0021 185.6863 0002194 286.1328 73.9282 15.27593455 09
| Epoch (UTC): | 25 May 2026 13:41:21 |
| Eccentricity: | 0.0002194 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 185.6863° |
| argument of perigee: | 286.1328° |
| revolutions per day: | 15.27593455 |
| mean anomaly at epoch: | 73.9282° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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