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 26088.22301139 +.00000000 +00000-0 +14042-3 0 00005
2 08294 81.2118 135.9357 0103807 350.9754 8.9546 14.09109241 04
| Epoch (UTC): | 29 March 2026 05:21:08 |
| Eccentricity: | 0.0103807 |
| inclination: | 81.2118° |
| perigee height: | 787 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 135.9357° |
| argument of perigee: | 350.9754° |
| revolutions per day: | 14.09109241 |
| mean anomaly at epoch: | 8.9546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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