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 68445U 26145.37142786 +.00000000 +00000-0 +19925-3 0 00005
2 68445 97.4508 104.0698 0006054 140.1417 220.0262 15.17169959 00
| Epoch (UTC): | 25 May 2026 08:54:51 |
| Eccentricity: | 0.0006054 |
| inclination: | 97.4508° |
| perigee height: | 510 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 104.0698° |
| argument of perigee: | 140.1417° |
| revolutions per day: | 15.17169959 |
| mean anomaly at epoch: | 220.0262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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