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 63194U 26145.58909536 +.00000000 +00000-0 +42157-3 0 00001
2 63194 43.0005 216.5304 0002196 240.2739 119.7910 15.70847921 05
| Epoch (UTC): | 25 May 2026 14:08:17 |
| Eccentricity: | 0.0002196 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 216.5304° |
| argument of perigee: | 240.2739° |
| revolutions per day: | 15.70847921 |
| mean anomaly at epoch: | 119.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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