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 07318U 26053.75608878 +.00000000 +00000-0 +00000-0 0 00007
2 07318 2.2245 251.9030 0031468 346.6654 250.3935 1.01980560 09
| Epoch (UTC): | 22 February 2026 18:08:46 |
| Eccentricity: | 0.0031468 |
| inclination: | 2.2245° |
| perigee height: | 35183 km |
| apogee height: | 35445 km |
| right ascension of ascending node: | 251.9030° |
| argument of perigee: | 346.6654° |
| revolutions per day: | 1.01980560 |
| mean anomaly at epoch: | 250.3935° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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