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 49271U 26145.51515770 +.00000000 +00000-0 +31299-1 0 00000
2 49271 51.6158 70.0245 0920219 233.1587 118.1415 12.41696160 08
| Epoch (UTC): | 25 May 2026 12:21:49 |
| Eccentricity: | 0.0920219 |
| inclination: | 51.6158° |
| perigee height: | 775 km |
| apogee height: | 2224 km |
| right ascension of ascending node: | 70.0245° |
| argument of perigee: | 233.1587° |
| revolutions per day: | 12.41696160 |
| mean anomaly at epoch: | 118.1415° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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