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 49202U 26145.48155762 +.00000000 +00000-0 +82699-3 0 00003
2 49202 87.8939 324.7520 0002132 100.0125 260.1244 13.13469235 09
| Epoch (UTC): | 25 May 2026 11:33:26 |
| Eccentricity: | 0.0002132 |
| inclination: | 87.8939° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7520° |
| argument of perigee: | 100.0125° |
| revolutions per day: | 13.13469235 |
| mean anomaly at epoch: | 260.1244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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