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 30579U 26018.56039127 +.00000000 +00000-0 +17347-3 0 00002
2 30579 98.8039 47.1674 0052613 1.2677 150.2923 14.05292682 03
| Epoch (UTC): | 18 January 2026 13:26:57 |
| Eccentricity: | 0.0052613 |
| inclination: | 98.8039° |
| perigee height: | 837 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 47.1674° |
| argument of perigee: | 1.2677° |
| revolutions per day: | 14.05292682 |
| mean anomaly at epoch: | 150.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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