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 63187U 26145.54144638 +.00000000 +00000-0 +12854-2 0 00003
2 63187 42.9993 217.0415 0001269 276.4344 83.6379 15.70852079 01
| Epoch (UTC): | 25 May 2026 12:59:40 |
| Eccentricity: | 0.0001269 |
| inclination: | 42.9993° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 217.0415° |
| argument of perigee: | 276.4344° |
| revolutions per day: | 15.70852079 |
| mean anomaly at epoch: | 83.6379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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