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 23405U 26088.05851976 +.00000000 +00000-0 -85772-5 0 00007
2 23405 70.9834 311.7427 0001931 196.9872 163.1187 14.15569231 02
| Epoch (UTC): | 29 March 2026 01:24:16 |
| Eccentricity: | 0.0001931 |
| inclination: | 70.9834° |
| perigee height: | 839 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 311.7427° |
| argument of perigee: | 196.9872° |
| revolutions per day: | 14.15569231 |
| mean anomaly at epoch: | 163.1187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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