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 26039.19832182 +.00000000 +00000-0 +11254-3 0 00003
2 11963 81.2779 302.7841 0075611 135.8381 224.8861 14.10155551 09
| Epoch (UTC): | 08 February 2026 04:45:35 |
| Eccentricity: | 0.0075611 |
| inclination: | 81.2779° |
| perigee height: | 804 km |
| apogee height: | 914 km |
| right ascension of ascending node: | 302.7841° |
| argument of perigee: | 135.8381° |
| revolutions per day: | 14.10155551 |
| mean anomaly at epoch: | 224.8861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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