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 26067.60510750 +.00000000 +00000-0 +13892-2 0 00008
2 38770 64.6221 231.5605 0023460 232.1623 127.7415 15.91845112 08
| Epoch (UTC): | 08 March 2026 14:31:21 |
| Eccentricity: | 0.0023460 |
| inclination: | 64.6221° |
| perigee height: | 281 km |
| apogee height: | 313 km |
| right ascension of ascending node: | 231.5605° |
| argument of perigee: | 232.1623° |
| revolutions per day: | 15.91845112 |
| mean anomaly at epoch: | 127.7415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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