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 23605U 26150.32624279 +.00000000 +00000-0 +23276-3 0 00001
2 23605 98.1982 39.5154 0013538 91.9333 268.3442 15.05654804 07
| Epoch (UTC): | 30 May 2026 07:49:47 |
| Eccentricity: | 0.0013538 |
| inclination: | 98.1982° |
| perigee height: | 540 km |
| apogee height: | 559 km |
| right ascension of ascending node: | 39.5154° |
| argument of perigee: | 91.9333° |
| revolutions per day: | 15.05654804 |
| mean anomaly at epoch: | 268.3442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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