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 26038.93472258 +.00000000 +00000-0 +95658-4 0 00007
2 12997 82.9652 335.9829 0058058 175.2175 255.6589 12.15869273 09
| Epoch (UTC): | 07 February 2026 22:26:00 |
| Eccentricity: | 0.0058058 |
| inclination: | 82.9652° |
| perigee height: | 1564 km |
| apogee height: | 1657 km |
| right ascension of ascending node: | 335.9829° |
| argument of perigee: | 175.2175° |
| revolutions per day: | 12.15869273 |
| mean anomaly at epoch: | 255.6589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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