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 10011U 26069.95654213 +.00000000 +00000-0 -52710-4 0 00004
2 10011 65.8629 282.6437 0692220 74.4550 21.1393 12.32266902 01
| Epoch (UTC): | 10 March 2026 22:57:25 |
| Eccentricity: | 0.0692220 |
| inclination: | 65.8629° |
| perigee height: | 991 km |
| apogee height: | 2088 km |
| right ascension of ascending node: | 282.6437° |
| argument of perigee: | 74.4550° |
| revolutions per day: | 12.32266902 |
| mean anomaly at epoch: | 21.1393° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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