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 26020.14946927 +.00000000 +00000-0 +27339-4 0 00004
2 23088 70.9999 172.8244 0003776 331.9746 28.1173 14.15006726 04
| Epoch (UTC): | 20 January 2026 03:35:14 |
| Eccentricity: | 0.0003776 |
| inclination: | 70.9999° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 172.8244° |
| argument of perigee: | 331.9746° |
| revolutions per day: | 14.15006726 |
| mean anomaly at epoch: | 28.1173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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