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 68313U 26145.32196105 +.00000000 +00000-0 +93944-3 0 00001
2 68313 97.2851 271.6520 0001258 71.4841 288.6561 15.75203608 02
| Epoch (UTC): | 25 May 2026 07:43:37 |
| Eccentricity: | 0.0001258 |
| inclination: | 97.2851° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6520° |
| argument of perigee: | 71.4841° |
| revolutions per day: | 15.75203608 |
| mean anomaly at epoch: | 288.6561° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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