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 38250U 26144.56254196 +.00000000 +00000-0 +00000-0 0 00006
2 38250 55.7786 305.6708 0019724 275.7368 84.0185 1.86229567 00
| Epoch (UTC): | 24 May 2026 13:30:03 |
| Eccentricity: | 0.0019724 |
| inclination: | 55.7786° |
| perigee height: | 21473 km |
| apogee height: | 21583 km |
| right ascension of ascending node: | 305.6708° |
| argument of perigee: | 275.7368° |
| revolutions per day: | 1.86229567 |
| mean anomaly at epoch: | 84.0185° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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