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 28158U 26152.06063522 +.00000000 +00000-0 +00000-0 0 00007
2 28158 12.0410 26.1915 0001344 319.4151 230.6547 1.00411742 01
| Epoch (UTC): | 01 June 2026 01:27:18 |
| Eccentricity: | 0.0001344 |
| inclination: | 12.0410° |
| perigee height: | 35742 km |
| apogee height: | 35753 km |
| right ascension of ascending node: | 26.1915° |
| argument of perigee: | 319.4151° |
| revolutions per day: | 1.00411742 |
| mean anomaly at epoch: | 230.6547° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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