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 26065.59357948 +.00000000 +00000-0 +12585-2 0 00000
2 38770 64.6222 238.8729 0024960 229.5274 130.3710 15.90058912 05
| Epoch (UTC): | 06 March 2026 14:14:45 |
| Eccentricity: | 0.0024960 |
| inclination: | 64.6222° |
| perigee height: | 285 km |
| apogee height: | 319 km |
| right ascension of ascending node: | 238.8729° |
| argument of perigee: | 229.5274° |
| revolutions per day: | 15.90058912 |
| mean anomaly at epoch: | 130.3710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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