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 38745U 26145.36399244 +.00000000 +00000-0 +58514-3 0 00004
2 38745 49.8220 137.9731 1576707 110.3028 267.3906 12.41676468 01
| Epoch (UTC): | 25 May 2026 08:44:08 |
| Eccentricity: | 0.1576707 |
| inclination: | 49.8220° |
| perigee height: | 257 km |
| apogee height: | 2742 km |
| right ascension of ascending node: | 137.9731° |
| argument of perigee: | 110.3028° |
| revolutions per day: | 12.41676468 |
| mean anomaly at epoch: | 267.3906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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