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 63680U 26145.50915097 +.00000000 +00000-0 +66824-3 0 00009
2 63680 43.0028 316.6320 0001016 275.7690 84.3046 15.27591160 09
| Epoch (UTC): | 25 May 2026 12:13:10 |
| Eccentricity: | 0.0001016 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 316.6320° |
| argument of perigee: | 275.7690° |
| revolutions per day: | 15.27591160 |
| mean anomaly at epoch: | 84.3046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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