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 54045U 26145.60923432 +.00000000 +00000-0 +51984-3 0 00008
2 54045 34.9893 221.1166 0006287 8.9059 351.1774 15.46947138 05
| Epoch (UTC): | 25 May 2026 14:37:17 |
| Eccentricity: | 0.0006287 |
| inclination: | 34.9893° |
| perigee height: | 421 km |
| apogee height: | 430 km |
| right ascension of ascending node: | 221.1166° |
| argument of perigee: | 8.9059° |
| revolutions per day: | 15.46947138 |
| mean anomaly at epoch: | 351.1774° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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