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 44517U 26145.59467744 +.00000000 +00000-0 +86452-4 0 00007
2 44517 99.2056 157.5361 0014864 229.0365 130.9505 13.85943392 02
| Epoch (UTC): | 25 May 2026 14:16:20 |
| Eccentricity: | 0.0014864 |
| inclination: | 99.2056° |
| perigee height: | 932 km |
| apogee height: | 954 km |
| right ascension of ascending node: | 157.5361° |
| argument of perigee: | 229.0365° |
| revolutions per day: | 13.85943392 |
| mean anomaly at epoch: | 130.9505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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