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 63193U 26145.55724382 +.00000000 +00000-0 +93804-3 0 00006
2 63193 43.0006 216.2741 0001526 289.1567 70.9136 15.70856965 00
| Epoch (UTC): | 25 May 2026 13:22:25 |
| Eccentricity: | 0.0001526 |
| inclination: | 43.0006° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 216.2741° |
| argument of perigee: | 289.1567° |
| revolutions per day: | 15.70856965 |
| mean anomaly at epoch: | 70.9136° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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