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 26039.49788532 +.00000000 +00000-0 +94484-3 0 00006
2 38770 64.6299 332.5911 0035040 222.3519 137.4929 15.77482986 05
| Epoch (UTC): | 08 February 2026 11:56:57 |
| Eccentricity: | 0.0035040 |
| inclination: | 64.6299° |
| perigee height: | 314 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 332.5911° |
| argument of perigee: | 222.3519° |
| revolutions per day: | 15.77482986 |
| mean anomaly at epoch: | 137.4929° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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