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 26066.14677124 +.00000000 +00000-0 +82042-3 0 00003
2 23608 98.2875 270.0170 0007443 45.2265 314.9586 15.46948857 02
| Epoch (UTC): | 07 March 2026 03:31:21 |
| Eccentricity: | 0.0007443 |
| inclination: | 98.2875° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 270.0170° |
| argument of perigee: | 45.2265° |
| revolutions per day: | 15.46948857 |
| mean anomaly at epoch: | 314.9586° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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