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 26063.76890344 +.00000000 +00000-0 +15727-2 0 00000
2 38770 64.6232 245.4925 0025945 226.6403 133.2595 15.88764517 09
| Epoch (UTC): | 04 March 2026 18:27:13 |
| Eccentricity: | 0.0025945 |
| inclination: | 64.6232° |
| perigee height: | 288 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 245.4925° |
| argument of perigee: | 226.6403° |
| revolutions per day: | 15.88764517 |
| mean anomaly at epoch: | 133.2595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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