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 41849U 26145.62863750 +.00000000 +00000-0 +71598-3 0 00007
2 41849 97.9926 32.6337 0007005 87.3259 272.8793 15.52296513 07
| Epoch (UTC): | 25 May 2026 15:05:14 |
| Eccentricity: | 0.0007005 |
| inclination: | 97.9926° |
| perigee height: | 405 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 32.6337° |
| argument of perigee: | 87.3259° |
| revolutions per day: | 15.52296513 |
| mean anomaly at epoch: | 272.8793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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