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 26040.95576987 +.00000000 +00000-0 +92349-3 0 00006
2 38770 64.6295 327.3949 0034756 221.9284 137.9208 15.77973987 02
| Epoch (UTC): | 09 February 2026 22:56:18 |
| Eccentricity: | 0.0034756 |
| inclination: | 64.6295° |
| perigee height: | 313 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 327.3949° |
| argument of perigee: | 221.9284° |
| revolutions per day: | 15.77973987 |
| mean anomaly at epoch: | 137.9208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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