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 68375U 26100.48207132 +.00000000 +00000-0 +32225-3 0 00005
2 68375 82.2954 88.5907 0021767 16.2857 343.9106 15.83519514 08
| Epoch (UTC): | 10 April 2026 11:34:10 |
| Eccentricity: | 0.0021767 |
| inclination: | 82.2954° |
| perigee height: | 306 km |
| apogee height: | 335 km |
| right ascension of ascending node: | 88.5907° |
| argument of perigee: | 16.2857° |
| revolutions per day: | 15.83519514 |
| mean anomaly at epoch: | 343.9106° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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