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 26018.66493458 +.00000000 +00000-0 +43179-4 0 00004
2 23088 70.9996 175.9421 0003663 333.8141 26.2795 14.15006582 06
| Epoch (UTC): | 18 January 2026 15:57:30 |
| Eccentricity: | 0.0003663 |
| inclination: | 70.9996° |
| perigee height: | 840 km |
| apogee height: | 845 km |
| right ascension of ascending node: | 175.9421° |
| argument of perigee: | 333.8141° |
| revolutions per day: | 14.15006582 |
| mean anomaly at epoch: | 26.2795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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