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 67069U 26145.02347970 +.00000000 +00000-0 +44906-3 0 00007
2 67069 41.3513 253.2926 0004039 319.3094 40.7425 15.16082859 08
| Epoch (UTC): | 25 May 2026 00:33:48 |
| Eccentricity: | 0.0004039 |
| inclination: | 41.3513° |
| perigee height: | 515 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 253.2926° |
| argument of perigee: | 319.3094° |
| revolutions per day: | 15.16082859 |
| mean anomaly at epoch: | 40.7425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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