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 54021U 26145.58715696 +.00000000 +00000-0 +14223-3 0 00005
2 54021 54.9998 305.1562 0015273 28.5310 331.6516 14.62252958 06
| Epoch (UTC): | 25 May 2026 14:05:30 |
| Eccentricity: | 0.0015273 |
| inclination: | 54.9998° |
| perigee height: | 675 km |
| apogee height: | 697 km |
| right ascension of ascending node: | 305.1562° |
| argument of perigee: | 28.5310° |
| revolutions per day: | 14.62252958 |
| mean anomaly at epoch: | 331.6516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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