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 49492U 26145.59286619 +.00000000 +00000-0 +21839-3 0 00001
2 49492 97.2102 190.6071 0009536 132.6700 227.5343 15.23640089 01
| Epoch (UTC): | 25 May 2026 14:13:43 |
| Eccentricity: | 0.0009536 |
| inclination: | 97.2102° |
| perigee height: | 488 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 190.6071° |
| argument of perigee: | 132.6700° |
| revolutions per day: | 15.23640089 |
| mean anomaly at epoch: | 227.5343° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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