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 68402U 26145.34933735 +.00000000 +00000-0 +69967-3 0 00008
2 68402 97.2842 287.9104 0001615 97.2293 262.9133 15.33465477 01
| Epoch (UTC): | 25 May 2026 08:23:02 |
| Eccentricity: | 0.0001615 |
| inclination: | 97.2842° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.9104° |
| argument of perigee: | 97.2293° |
| revolutions per day: | 15.33465477 |
| mean anomaly at epoch: | 262.9133° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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