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 12785U 26038.43640453 +.00000000 +00000-0 +12903-3 0 00002
2 12785 82.4521 143.0866 0011333 282.9710 77.0328 16.50758067 07
| Epoch (UTC): | 07 February 2026 10:28:25 |
| Eccentricity: | 0.0011333 |
| inclination: | 82.4521° |
| perigee height: | 130 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 143.0866° |
| argument of perigee: | 282.9710° |
| revolutions per day: | 16.50758067 |
| mean anomaly at epoch: | 77.0328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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