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 06824U 26088.11407037 +.00000000 +00000-0 +24067-3 0 00002
2 06824 95.5031 142.4945 0007348 148.2785 239.5370 12.56488397 03
| Epoch (UTC): | 29 March 2026 02:44:15 |
| Eccentricity: | 0.0007348 |
| inclination: | 95.5031° |
| perigee height: | 1432 km |
| apogee height: | 1443 km |
| right ascension of ascending node: | 142.4945° |
| argument of perigee: | 148.2785° |
| revolutions per day: | 12.56488397 |
| mean anomaly at epoch: | 239.5370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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