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 68307U 26145.58335647 +.00000000 +00000-0 -55578-3 0 00000
2 68307 97.2842 271.8140 0001416 90.9925 44.4364 15.75212718 01
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001416 |
| inclination: | 97.2842° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.8140° |
| argument of perigee: | 90.9925° |
| revolutions per day: | 15.75212718 |
| mean anomaly at epoch: | 44.4364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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