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 68022U 26145.37828434 +.00000000 +00000-0 +60281-3 0 00008
2 68022 97.2845 94.3553 0002523 111.7364 248.4148 15.33452542 04
| Epoch (UTC): | 25 May 2026 09:04:43 |
| Eccentricity: | 0.0002523 |
| inclination: | 97.2845° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3553° |
| argument of perigee: | 111.7364° |
| revolutions per day: | 15.33452542 |
| mean anomaly at epoch: | 248.4148° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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