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 26065.24116339 +.00000000 +00000-0 +81666-3 0 00000
2 23608 98.2874 268.9814 0007460 47.9845 312.2036 15.46871866 00
| Epoch (UTC): | 06 March 2026 05:47:16 |
| Eccentricity: | 0.0007460 |
| inclination: | 98.2874° |
| perigee height: | 421 km |
| apogee height: | 431 km |
| right ascension of ascending node: | 268.9814° |
| argument of perigee: | 47.9845° |
| revolutions per day: | 15.46871866 |
| mean anomaly at epoch: | 312.2036° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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