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 52159U 26052.49997748 +.00000000 +00000-0 +30517-4 0 00007
2 52159 97.9792 136.3952 0001114 75.3243 284.8089 14.74945591 05
| Epoch (UTC): | 21 February 2026 11:59:58 |
| Eccentricity: | 0.0001114 |
| inclination: | 97.9792° |
| perigee height: | 645 km |
| apogee height: | 646 km |
| right ascension of ascending node: | 136.3952° |
| argument of perigee: | 75.3243° |
| revolutions per day: | 14.74945591 |
| mean anomaly at epoch: | 284.8089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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