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 26100.15192887 +.00000000 +00000-0 +51217-4 0 00006
2 08294 81.2104 124.2986 0103696 316.8697 42.4381 14.09113896 02
| Epoch (UTC): | 10 April 2026 03:38:46 |
| Eccentricity: | 0.0103696 |
| inclination: | 81.2104° |
| perigee height: | 787 km |
| apogee height: | 937 km |
| right ascension of ascending node: | 124.2986° |
| argument of perigee: | 316.8697° |
| revolutions per day: | 14.09113896 |
| mean anomaly at epoch: | 42.4381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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