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 49962U 26145.74202919 +.00000000 +00000-0 +10651-3 0 00001
2 49962 97.3779 127.1327 0003120 100.2325 259.9258 15.11778510 02
| Epoch (UTC): | 25 May 2026 17:48:31 |
| Eccentricity: | 0.0003120 |
| inclination: | 97.3779° |
| perigee height: | 529 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 127.1327° |
| argument of perigee: | 100.2325° |
| revolutions per day: | 15.11778510 |
| mean anomaly at epoch: | 259.9258° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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