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 68150U 26145.32338882 +.00000000 +00000-0 +35727-3 0 00005
2 68150 97.2857 167.0107 0001197 99.7525 260.3853 15.33452610 04
| Epoch (UTC): | 25 May 2026 07:45:40 |
| Eccentricity: | 0.0001197 |
| inclination: | 97.2857° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.0107° |
| argument of perigee: | 99.7525° |
| revolutions per day: | 15.33452610 |
| mean anomaly at epoch: | 260.3853° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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