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 68366U 26145.20887873 +.00000000 +00000-0 +41291-3 0 00003
2 68366 82.2971 38.3299 0003230 174.3474 185.7823 15.66414975 04
| Epoch (UTC): | 25 May 2026 05:00:47 |
| Eccentricity: | 0.0003230 |
| inclination: | 82.2971° |
| perigee height: | 367 km |
| apogee height: | 371 km |
| right ascension of ascending node: | 38.3299° |
| argument of perigee: | 174.3474° |
| revolutions per day: | 15.66414975 |
| mean anomaly at epoch: | 185.7823° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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