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 68649U 26144.78333637 +.00000000 +00000-0 +40695-4 0 00001
2 68649 88.9875 323.3927 0009001 64.9511 295.2582 13.65684381 03
| Epoch (UTC): | 24 May 2026 18:48:00 |
| Eccentricity: | 0.0009001 |
| inclination: | 88.9875° |
| perigee height: | 1008 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 323.3927° |
| argument of perigee: | 64.9511° |
| revolutions per day: | 13.65684381 |
| mean anomaly at epoch: | 295.2582° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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