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 26038.16552387 +.00000000 +00000-0 +11103-2 0 00004
2 38745 49.8276 122.0718 1611708 182.4185 176.8057 12.33850249 00
| Epoch (UTC): | 07 February 2026 03:58:21 |
| Eccentricity: | 0.1611708 |
| inclination: | 49.8276° |
| perigee height: | 258 km |
| apogee height: | 2808 km |
| right ascension of ascending node: | 122.0718° |
| argument of perigee: | 182.4185° |
| revolutions per day: | 12.33850249 |
| mean anomaly at epoch: | 176.8057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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