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 68208U 26145.09454635 +.00000000 +00000-0 +52453-3 0 00003
2 68208 97.2867 20.4885 0001746 94.8389 265.3053 15.33449306 03
| Epoch (UTC): | 25 May 2026 02:16:08 |
| Eccentricity: | 0.0001746 |
| inclination: | 97.2867° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.4885° |
| argument of perigee: | 94.8389° |
| revolutions per day: | 15.33449306 |
| mean anomaly at epoch: | 265.3053° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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