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 26064.71287757 +.00000000 +00000-0 +12283-2 0 00008
2 38770 64.6230 242.0692 0025454 228.3238 131.5743 15.89468610 03
| Epoch (UTC): | 05 March 2026 17:06:32 |
| Eccentricity: | 0.0025454 |
| inclination: | 64.6230° |
| perigee height: | 287 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 242.0692° |
| argument of perigee: | 228.3238° |
| revolutions per day: | 15.89468610 |
| mean anomaly at epoch: | 131.5743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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