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 08294U 26074.94493873 +.00000000 +00000-0 +18527-3 0 00008
2 08294 81.2130 148.8858 0104363 28.5735 332.1099 14.09101051 08
| Epoch (UTC): | 15 March 2026 22:40:42 |
| Eccentricity: | 0.0104363 |
| inclination: | 81.2130° |
| perigee height: | 787 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 148.8858° |
| argument of perigee: | 28.5735° |
| revolutions per day: | 14.09101051 |
| mean anomaly at epoch: | 332.1099° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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