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 12964U 26110.90820600 +.00000000 +00000-0 +19361-4 0 00004
2 12964 82.9462 158.8126 0037441 297.4849 242.5521 13.80312231 03
| Epoch (UTC): | 20 April 2026 21:47:48 |
| Eccentricity: | 0.0037441 |
| inclination: | 82.9462° |
| perigee height: | 935 km |
| apogee height: | 990 km |
| right ascension of ascending node: | 158.8126° |
| argument of perigee: | 297.4849° |
| revolutions per day: | 13.80312231 |
| mean anomaly at epoch: | 242.5521° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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