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 12649U 26101.37739762 +.00000000 +00000-0 +31532-3 0 00006
2 12649 82.9161 244.0596 0047215 339.1240 49.8005 13.81404381 01
| Epoch (UTC): | 11 April 2026 09:03:27 |
| Eccentricity: | 0.0047215 |
| inclination: | 82.9161° |
| perigee height: | 924 km |
| apogee height: | 994 km |
| right ascension of ascending node: | 244.0596° |
| argument of perigee: | 339.1240° |
| revolutions per day: | 13.81404381 |
| mean anomaly at epoch: | 49.8005° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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