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 38552U 26145.08466622 +.00000000 +00000-0 +00000-0 0 00008
2 38552 4.6194 61.1269 0001910 325.7927 246.2972 1.00273267 00
| Epoch (UTC): | 25 May 2026 02:01:55 |
| Eccentricity: | 0.0001910 |
| inclination: | 4.6194° |
| perigee height: | 35778 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 61.1269° |
| argument of perigee: | 325.7927° |
| revolutions per day: | 1.00273267 |
| mean anomaly at epoch: | 246.2972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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