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 68824U 26145.29296088 +.00000000 +00000-0 +14017-2 0 00008
2 68824 97.2848 351.9768 0001397 74.7749 285.3671 15.75243420 00
| Epoch (UTC): | 25 May 2026 07:01:51 |
| Eccentricity: | 0.0001397 |
| inclination: | 97.2848° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 351.9768° |
| argument of perigee: | 74.7749° |
| revolutions per day: | 15.75243420 |
| mean anomaly at epoch: | 285.3671° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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