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 26064.91772125 +.00000000 +00000-0 +82965-3 0 00007
2 23608 98.2875 268.6115 0007454 49.0205 311.1686 15.46845137 09
| Epoch (UTC): | 05 March 2026 22:01:31 |
| Eccentricity: | 0.0007454 |
| inclination: | 98.2875° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 268.6115° |
| argument of perigee: | 49.0205° |
| revolutions per day: | 15.46845137 |
| mean anomaly at epoch: | 311.1686° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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