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 67079U 26145.54742020 +.00000000 +00000-0 +16791-3 0 00001
2 67079 70.0014 180.5303 0003761 267.4896 92.5832 14.98334262 03
| Epoch (UTC): | 25 May 2026 13:08:17 |
| Eccentricity: | 0.0003761 |
| inclination: | 70.0014° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 180.5303° |
| argument of perigee: | 267.4896° |
| revolutions per day: | 14.98334262 |
| mean anomaly at epoch: | 92.5832° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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