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 68302U 26145.32619556 +.00000000 +00000-0 +10221-2 0 00005
2 68302 97.2842 271.6478 0001223 55.5555 304.5826 15.75205221 04
| Epoch (UTC): | 25 May 2026 07:49:43 |
| Eccentricity: | 0.0001223 |
| inclination: | 97.2842° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6478° |
| argument of perigee: | 55.5555° |
| revolutions per day: | 15.75205221 |
| mean anomaly at epoch: | 304.5826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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