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 26071.99744250 +.00000000 +00000-0 +97126-3 0 00002
2 38770 64.6203 215.5259 0020520 239.7398 120.1733 15.95707631 08
| Epoch (UTC): | 12 March 2026 23:56:19 |
| Eccentricity: | 0.0020520 |
| inclination: | 64.6203° |
| perigee height: | 273 km |
| apogee height: | 300 km |
| right ascension of ascending node: | 215.5259° |
| argument of perigee: | 239.7398° |
| revolutions per day: | 15.95707631 |
| mean anomaly at epoch: | 120.1733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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