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 38770U 26041.96967454 +.00000000 +00000-0 +10368-2 0 00001
2 38770 64.6299 323.7770 0034293 221.8051 138.0483 15.78340426 09
| Epoch (UTC): | 10 February 2026 23:16:19 |
| Eccentricity: | 0.0034293 |
| inclination: | 64.6299° |
| perigee height: | 312 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 323.7770° |
| argument of perigee: | 221.8051° |
| revolutions per day: | 15.78340426 |
| mean anomaly at epoch: | 138.0483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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