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 26073.58382740 +.00000000 +00000-0 +99381-3 0 00000
2 23608 98.2875 278.5275 0007160 19.8782 340.2743 15.47625206 06
| Epoch (UTC): | 14 March 2026 14:00:42 |
| Eccentricity: | 0.0007160 |
| inclination: | 98.2875° |
| perigee height: | 419 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 278.5275° |
| argument of perigee: | 19.8782° |
| revolutions per day: | 15.47625206 |
| mean anomaly at epoch: | 340.2743° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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