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 63811U 26145.58335647 +.00000000 +00000-0 +89602-3 0 00009
2 63811 42.9845 60.6850 0024629 216.1810 92.2150 15.98681989 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0024629 |
| inclination: | 42.9845° |
| perigee height: | 262 km |
| apogee height: | 294 km |
| right ascension of ascending node: | 60.6850° |
| argument of perigee: | 216.1810° |
| revolutions per day: | 15.98681989 |
| mean anomaly at epoch: | 92.2150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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