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 23608U 26040.70868971 +.00000000 +00000-0 +80283-3 0 00004
2 23608 98.2894 240.9622 0007441 129.2465 230.9442 15.44967806 05
| Epoch (UTC): | 09 February 2026 17:00:30 |
| Eccentricity: | 0.0007441 |
| inclination: | 98.2894° |
| perigee height: | 426 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 240.9622° |
| argument of perigee: | 129.2465° |
| revolutions per day: | 15.44967806 |
| mean anomaly at epoch: | 230.9442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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