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 26064.58703755 +.00000000 +00000-0 +12646-2 0 00007
2 38770 64.6228 242.5262 0025526 228.2287 131.6691 15.89383469 02
| Epoch (UTC): | 05 March 2026 14:05:20 |
| Eccentricity: | 0.0025526 |
| inclination: | 64.6228° |
| perigee height: | 287 km |
| apogee height: | 321 km |
| right ascension of ascending node: | 242.5262° |
| argument of perigee: | 228.2287° |
| revolutions per day: | 15.89383469 |
| mean anomaly at epoch: | 131.6691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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