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 68104U 26145.38416075 +.00000000 +00000-0 +83608-3 0 00002
2 68104 97.2833 105.9631 0002492 111.9720 248.1787 15.33448081 00
| Epoch (UTC): | 25 May 2026 09:13:11 |
| Eccentricity: | 0.0002492 |
| inclination: | 97.2833° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 105.9631° |
| argument of perigee: | 111.9720° |
| revolutions per day: | 15.33448081 |
| mean anomaly at epoch: | 248.1787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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