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 26157.14424650 +.00000000 +00000-0 +89423-3 0 00008
2 23608 98.2739 14.5602 0007430 87.6498 272.5604 15.53963942 06
| Epoch (UTC): | 06 June 2026 03:27:42 |
| Eccentricity: | 0.0007430 |
| inclination: | 98.2739° |
| perigee height: | 400 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 14.5602° |
| argument of perigee: | 87.6498° |
| revolutions per day: | 15.53963942 |
| mean anomaly at epoch: | 272.5604° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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