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 11971U 26088.03088316 +.00000000 +00000-0 +30396-4 0 00000
2 11971 64.8327 294.9089 0049837 244.3344 270.6740 13.96930062 02
| Epoch (UTC): | 29 March 2026 00:44:28 |
| Eccentricity: | 0.0049837 |
| inclination: | 64.8327° |
| perigee height: | 868 km |
| apogee height: | 941 km |
| right ascension of ascending node: | 294.9089° |
| argument of perigee: | 244.3344° |
| revolutions per day: | 13.96930062 |
| mean anomaly at epoch: | 270.6740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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