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 38251U 26144.49480453 +.00000000 +00000-0 +00000-0 0 00006
2 38251 55.6787 304.8888 0010979 279.4145 80.4412 1.86229229 06
| Epoch (UTC): | 24 May 2026 11:52:31 |
| Eccentricity: | 0.0010979 |
| inclination: | 55.6787° |
| perigee height: | 21498 km |
| apogee height: | 21559 km |
| right ascension of ascending node: | 304.8888° |
| argument of perigee: | 279.4145° |
| revolutions per day: | 1.86229229 |
| mean anomaly at epoch: | 80.4412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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