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 10600U 26088.12634453 +.00000000 +00000-0 +33300-4 0 00005
2 10600 82.9403 48.6380 0046741 304.8942 54.7827 13.78838704 08
| Epoch (UTC): | 29 March 2026 03:01:56 |
| Eccentricity: | 0.0046741 |
| inclination: | 82.9403° |
| perigee height: | 934 km |
| apogee height: | 1002 km |
| right ascension of ascending node: | 48.6380° |
| argument of perigee: | 304.8942° |
| revolutions per day: | 13.78838704 |
| mean anomaly at epoch: | 54.7827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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