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 26075.93902278 +.00000000 +00000-0 +18765-3 0 00006
2 08294 81.2129 147.9163 0104322 25.7770 334.8546 14.09101736 04
| Epoch (UTC): | 16 March 2026 22:32:11 |
| Eccentricity: | 0.0104322 |
| inclination: | 81.2129° |
| perigee height: | 787 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 147.9163° |
| argument of perigee: | 25.7770° |
| revolutions per day: | 14.09101736 |
| mean anomaly at epoch: | 334.8546° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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