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 10974U 26109.09634090 +.00000000 +00000-0 +32520-4 0 00009
2 10974 82.4829 348.6180 0017973 76.3641 283.9578 14.90053303 00
| Epoch (UTC): | 19 April 2026 02:18:43 |
| Eccentricity: | 0.0017973 |
| inclination: | 82.4829° |
| perigee height: | 585 km |
| apogee height: | 610 km |
| right ascension of ascending node: | 348.6180° |
| argument of perigee: | 76.3641° |
| revolutions per day: | 14.90053303 |
| mean anomaly at epoch: | 283.9578° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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