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 23233U 26140.57840404 +.00000000 +00000-0 +69907-5 0 00007
2 23233 98.6706 191.5440 0010804 358.3406 1.7731 14.16068689 05
| Epoch (UTC): | 20 May 2026 13:52:54 |
| Eccentricity: | 0.0010804 |
| inclination: | 98.6706° |
| perigee height: | 831 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 191.5440° |
| argument of perigee: | 358.3406° |
| revolutions per day: | 14.16068689 |
| mean anomaly at epoch: | 1.7731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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