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 11964U 26106.89684543 +.00000000 +00000-0 +00000-0 0 00006
2 11964 8.1181 303.4338 0032918 105.2314 263.7787 0.99233968 04
| Epoch (UTC): | 16 April 2026 21:31:27 |
| Eccentricity: | 0.0032918 |
| inclination: | 8.1181° |
| perigee height: | 35940 km |
| apogee height: | 36220 km |
| right ascension of ascending node: | 303.4338° |
| argument of perigee: | 105.2314° |
| revolutions per day: | 0.99233968 |
| mean anomaly at epoch: | 263.7787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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