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 12508U 26039.83821704 +.00000000 +00000-0 +70177-4 0 00008
2 12508 82.9617 322.9081 0037864 13.0991 347.1140 13.76631367 00
| Epoch (UTC): | 08 February 2026 20:07:01 |
| Eccentricity: | 0.0037864 |
| inclination: | 82.9617° |
| perigee height: | 948 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 322.9081° |
| argument of perigee: | 13.0991° |
| revolutions per day: | 13.76631367 |
| mean anomaly at epoch: | 347.1140° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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