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 26017.88732134 +.00000000 +00000-0 +62236-4 0 00009
2 23088 70.9996 177.5749 0003588 334.8690 25.2257 14.15006449 07
| Epoch (UTC): | 17 January 2026 21:17:44 |
| Eccentricity: | 0.0003588 |
| inclination: | 70.9996° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 177.5749° |
| argument of perigee: | 334.8690° |
| revolutions per day: | 14.15006449 |
| mean anomaly at epoch: | 25.2257° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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