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 68143U 26145.01614419 +.00000000 +00000-0 +35668-3 0 00000
2 68143 97.2856 166.6605 0000761 105.1718 254.9608 15.33446582 03
| Epoch (UTC): | 25 May 2026 00:23:14 |
| Eccentricity: | 0.0000761 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 166.6605° |
| argument of perigee: | 105.1718° |
| revolutions per day: | 15.33446582 |
| mean anomaly at epoch: | 254.9608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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