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 26017.24747309 +.00000000 +00000-0 +80443-3 0 00006
2 23608 98.2885 214.2417 0007162 217.1393 142.9357 15.42878736 06
| Epoch (UTC): | 17 January 2026 05:56:21 |
| Eccentricity: | 0.0007162 |
| inclination: | 98.2885° |
| perigee height: | 433 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 214.2417° |
| argument of perigee: | 217.1393° |
| revolutions per day: | 15.42878736 |
| mean anomaly at epoch: | 142.9357° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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