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 68065U 26145.46287199 +.00000000 +00000-0 +57879-3 0 00001
2 68065 53.1607 53.1865 0001287 93.7645 266.3503 15.30203306 07
| Epoch (UTC): | 25 May 2026 11:06:32 |
| Eccentricity: | 0.0001287 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.1865° |
| argument of perigee: | 93.7645° |
| revolutions per day: | 15.30203306 |
| mean anomaly at epoch: | 266.3503° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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