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 67859U 26145.42672551 +.00000000 +00000-0 +31743-3 0 00009
2 67859 53.1601 207.1523 0001000 102.0342 258.0772 15.31695587 07
| Epoch (UTC): | 25 May 2026 10:14:29 |
| Eccentricity: | 0.0001000 |
| inclination: | 53.1601° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 207.1523° |
| argument of perigee: | 102.0342° |
| revolutions per day: | 15.31695587 |
| mean anomaly at epoch: | 258.0772° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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