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 23088U 26071.96673404 +.00000000 +00000-0 -82170-4 0 00002
2 23088 70.9985 64.0041 0005679 282.5687 77.4800 14.15010758 09
| Epoch (UTC): | 12 March 2026 23:12:05 |
| Eccentricity: | 0.0005679 |
| inclination: | 70.9985° |
| perigee height: | 838 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 64.0041° |
| argument of perigee: | 282.5687° |
| revolutions per day: | 14.15010758 |
| mean anomaly at epoch: | 77.4800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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