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 68222U 26145.64377727 +.00000000 +00000-0 +46972-3 0 00005
2 68222 97.2864 21.1194 0001666 87.7605 272.3828 15.33453897 08
| Epoch (UTC): | 25 May 2026 15:27:02 |
| Eccentricity: | 0.0001666 |
| inclination: | 97.2864° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.1194° |
| argument of perigee: | 87.7605° |
| revolutions per day: | 15.33453897 |
| mean anomaly at epoch: | 272.3828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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