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 11963U 26039.83690953 +.00000000 +00000-0 +11190-3 0 00001
2 11963 81.2778 302.1648 0075670 134.0280 226.7160 14.10155803 04
| Epoch (UTC): | 08 February 2026 20:05:08 |
| Eccentricity: | 0.0075670 |
| inclination: | 81.2778° |
| perigee height: | 804 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 302.1648° |
| argument of perigee: | 134.0280° |
| revolutions per day: | 14.10155803 |
| mean anomaly at epoch: | 226.7160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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