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 63842U 26145.61101569 +.00000000 +00000-0 +58542-3 0 00000
2 63842 43.0004 3.7189 0001512 227.5014 132.5710 15.27585199 05
| Epoch (UTC): | 25 May 2026 14:39:51 |
| Eccentricity: | 0.0001512 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 3.7189° |
| argument of perigee: | 227.5014° |
| revolutions per day: | 15.27585199 |
| mean anomaly at epoch: | 132.5710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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