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 23538U 26064.54690416 +.00000000 +00000-0 +16500-2 0 00001
2 23538 6.4432 269.1690 6044751 197.9736 124.4084 3.96394157 04
| Epoch (UTC): | 05 March 2026 13:07:32 |
| Eccentricity: | 0.6044751 |
| inclination: | 6.4432° |
| perigee height: | 292 km |
| apogee height: | 20681 km |
| right ascension of ascending node: | 269.1690° |
| argument of perigee: | 197.9736° |
| revolutions per day: | 3.96394157 |
| mean anomaly at epoch: | 124.4084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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