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 12997U 26105.58222580 +.00000000 +00000-0 +38254-3 0 00002
2 12997 82.9561 299.0081 0058860 37.2845 18.8883 12.15870839 06
| Epoch (UTC): | 15 April 2026 13:58:24 |
| Eccentricity: | 0.0058860 |
| inclination: | 82.9561° |
| perigee height: | 1564 km |
| apogee height: | 1658 km |
| right ascension of ascending node: | 299.0081° |
| argument of perigee: | 37.2845° |
| revolutions per day: | 12.15870839 |
| mean anomaly at epoch: | 18.8883° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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