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 63027U 26145.11755244 +.00000000 +00000-0 +34588-3 0 00009
2 63027 59.0000 49.3978 0014291 54.6532 305.5878 15.38942201 07
| Epoch (UTC): | 25 May 2026 02:49:16 |
| Eccentricity: | 0.0014291 |
| inclination: | 59.0000° |
| perigee height: | 439 km |
| apogee height: | 459 km |
| right ascension of ascending node: | 49.3978° |
| argument of perigee: | 54.6532° |
| revolutions per day: | 15.38942201 |
| mean anomaly at epoch: | 305.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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