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 67862U 26145.57189019 +.00000000 +00000-0 +61720-3 0 00009
2 67862 53.1582 207.3533 0000970 57.5122 302.5972 15.30208623 04
| Epoch (UTC): | 25 May 2026 13:43:31 |
| Eccentricity: | 0.0000970 |
| inclination: | 53.1582° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.3533° |
| argument of perigee: | 57.5122° |
| revolutions per day: | 15.30208623 |
| mean anomaly at epoch: | 302.5972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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