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 26040.85576265 +.00000000 +00000-0 +56498-4 0 00001
2 12508 82.9617 322.1541 0037803 10.2911 349.9012 13.76631460 09
| Epoch (UTC): | 09 February 2026 20:32:17 |
| Eccentricity: | 0.0037803 |
| inclination: | 82.9617° |
| perigee height: | 948 km |
| apogee height: | 1004 km |
| right ascension of ascending node: | 322.1541° |
| argument of perigee: | 10.2911° |
| revolutions per day: | 13.76631460 |
| mean anomaly at epoch: | 349.9012° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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