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 49949U 26145.56035164 +.00000000 +00000-0 +37840-3 0 00001
2 49949 41.9940 183.9973 0011730 95.6048 264.6134 15.50986022 02
| Epoch (UTC): | 25 May 2026 13:26:54 |
| Eccentricity: | 0.0011730 |
| inclination: | 41.9940° |
| perigee height: | 406 km |
| apogee height: | 422 km |
| right ascension of ascending node: | 183.9973° |
| argument of perigee: | 95.6048° |
| revolutions per day: | 15.50986022 |
| mean anomaly at epoch: | 264.6134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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