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 63079U 26145.45940309 +.00000000 +00000-0 +26174-3 0 00003
2 63079 70.0001 160.7977 0004104 267.0763 92.9927 14.98337878 08
| Epoch (UTC): | 25 May 2026 11:01:32 |
| Eccentricity: | 0.0004104 |
| inclination: | 70.0001° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.7977° |
| argument of perigee: | 267.0763° |
| revolutions per day: | 14.98337878 |
| mean anomaly at epoch: | 92.9927° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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