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 12848U 26021.49840801 +.00000000 +00000-0 +56109-3 0 00005
2 12848 82.4685 61.5373 0467401 303.4192 52.3117 14.56522189 09
| Epoch (UTC): | 21 January 2026 11:57:42 |
| Eccentricity: | 0.0467401 |
| inclination: | 82.4685° |
| perigee height: | 373 km |
| apogee height: | 1035 km |
| right ascension of ascending node: | 61.5373° |
| argument of perigee: | 303.4192° |
| revolutions per day: | 14.56522189 |
| mean anomaly at epoch: | 52.3117° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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